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SPACEMOBILE-003

SPACEMOBILE-003 is one of AST SpaceMobile's first five commercial BlueBird satellites, launched together in September 2024. The BlueBird system is designed to connect ordinary cellular devices through large phased-array antennas in low Earth orbit, working with terrestrial mobile-network partners rather than requiring a specialized satellite handset. The mission illustrates how satellite communications and existing cellular standards are beginning to overlap.

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Object identity

NORAD ID
61045
COSPAR ID
2024-163A
Operator
Not listed
Country
Not listed
Launch date
Not listed

Immediate discovery

Why this satellite matters

A radio link weakens greatly as distance increases. A space-to-phone system must balance transmitted power, antenna gain, frequency, bandwidth, atmospheric losses and the small antenna inside an ordinary mobile device.

Understanding the mission

Science and engineering ideas

A radio link weakens greatly as distance increases. A space-to-phone system must balance transmitted power, antenna gain, frequency, bandwidth, atmospheric losses and the small antenna inside an ordinary mobile device.

AST SpaceMobile reports a phased-array area of approximately 64.4 square meters (693 square feet) for each of the first five BlueBird satellites. A large array can concentrate radio energy electronically and form beams toward selected service areas without mechanically pointing the entire spacecraft.

Low Earth orbit reduces signal travel distance and latency compared with geostationary orbit, but each spacecraft sees a smaller part of Earth and moves quickly across the sky. Continuous service therefore requires a coordinated constellation rather than one satellite.

Frequency coordination and partnerships with terrestrial mobile operators are essential because the satellite system must work within regulated spectrum and existing cellular networks.

TransitSatellite calculates altitude, speed and orbital period from the current catalog data. Those values change over time and are separate from company claims about network performance.

Mission

Mission and purpose

The current public orbital catalog identifies this object, but verified mission-specific information may be limited. TransitSatellite will expand this page when authoritative information is available.

  • A radio link weakens greatly as distance increases. A space-to-phone system must balance transmitted power, antenna gain, frequency, bandwidth, atmospheric losses and the small antenna inside an ordinary mobile device.
  • AST SpaceMobile reports a phased-array area of approximately 64.4 square meters (693 square feet) for each of the first five BlueBird satellites. A large array can concentrate radio energy electronically and form beams toward selected service areas without mechanically pointing the entire spacecraft.
  • Low Earth orbit reduces signal travel distance and latency compared with geostationary orbit, but each spacecraft sees a smaller part of Earth and moves quickly across the sky. Continuous service therefore requires a coordinated constellation rather than one satellite.
  • Frequency coordination and partnerships with terrestrial mobile operators are essential because the satellite system must work within regulated spectrum and existing cellular networks.
  • TransitSatellite calculates altitude, speed and orbital period from the current catalog data. Those values change over time and are separate from company claims about network performance.

Design

Engineering

A radio link weakens greatly as distance increases. A space-to-phone system must balance transmitted power, antenna gain, frequency, bandwidth, atmospheric losses and the small antenna inside an ordinary mobile device. AST SpaceMobile reports a phased-array area of approximately 64.4 square meters (693 square feet) for each of the first five BlueBird satellites. A large array can concentrate radio energy electronically and form beams toward selected service areas without mechanically pointing the entire spacecraft. Low Earth orbit reduces signal travel distance and latency compared with geostationary orbit, but each spacecraft sees a smaller part of Earth and moves quickly across the sky. Continuous service therefore requires a coordinated constellation rather than one satellite. Frequency coordination and partnerships with terrestrial mobile operators are essential because the satellite system must work within regulated spectrum and existing cellular networks. TransitSatellite calculates altitude, speed and orbital period from the current catalog data. Those values change over time and are separate from company claims about network performance.

Real orbital values

The mathematics

The current two-line element set reports approximately 15.2041 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 94.7 minutes.

Period

94.7 min

Representative speed

27,396 km/h

Representative altitude

512 km

Inclination

52.97°

These are representative calculations derived from current orbital elements, not fixed physical specifications. Altitude and speed change around an elliptical orbit, and predictions change as new orbital elements are published.

Launch record

Launch and deployment

SPACEMOBILE-003 launched with four companion BlueBird satellites on 12 September 2024 aboard a SpaceX Falcon 9 from Cape Canaveral, Florida. The five satellites were released into low Earth orbit and later unfolded their large communications arrays. They form the company's first commercial group of BlueBird spacecraft and were designed to provide non-continuous service while additional satellites are deployed.

TransitSatellite does not estimate historical launch weather. Temperature, clouds, wind, holds, and scrub reasons will appear only when supported by traceable historical sources.

Orbit

LEO orbit explained

Low Earth orbit is the region closest to Earth used by most crewed spacecraft, many science missions, Earth-observation satellites, and large constellations. Objects move quickly and commonly complete an orbit in roughly 90 to 130 minutes.

LEO can provide detailed Earth views, lower communications delay, and easier access than higher orbits, but it covers less area per spacecraft and is more affected by atmospheric drag.

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Learning

Questions to explore

  • What can an orbit tell us before the mission is fully identified?
  • Why are stable catalog identifiers important?

Evidence

Sources and data notes

Current identity and orbital elements come from CelesTrak’s public GP data. Calculated orbit values are derived from the current TLE and may change after catalog updates. Mission-history claims are added separately and require authoritative sources.

Catalog updated

Sep 19, 2026, 2:53 PM UTC

Story review

2026-08-30