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TIANZHOU-10

TIANZHOU-10 is a Tianzhou cargo spacecraft supporting China's Tiangong space station. Tianzhou vehicles deliver supplies and propellant and are an essential part of sustaining long-duration crewed operations.

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Object identity

NORAD ID
69049
COSPAR ID
2026-102A
Operator
Not listed
Country
Not listed
Launch date
Not listed

Immediate discovery

Why this satellite matters

Tianzhou provides a useful comparison with Progress and Cygnus: different spacecraft and launch systems solve the same orbital logistics problem of delivering mass to a moving station.

Understanding the mission

Science and engineering ideas

Tianzhou provides a useful comparison with Progress and Cygnus: different spacecraft and launch systems solve the same orbital logistics problem of delivering mass to a moving station.

Mission

Mission and purpose

Objects in this category may be crewed stations, modules, cargo vehicles, or other spacecraft directly connected with human activity in orbit. The exact role depends on the individual object.

  • Tianzhou provides a useful comparison with Progress and Cygnus: different spacecraft and launch systems solve the same orbital logistics problem of delivering mass to a moving station.

Design

Engineering

Tianzhou provides a useful comparison with Progress and Cygnus: different spacecraft and launch systems solve the same orbital logistics problem of delivering mass to a moving station.

Real orbital values

The mathematics

The current two-line element set reports approximately 15.6009 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 92.3 minutes.

Period

92.3 min

Representative speed

27,633 km/h

Representative altitude

395 km

Inclination

41.47°

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

The orbital catalog lists the launch designator as 2026-102A. A fully sourced launch story, launch vehicle, deployment sequence, historical weather, and documented delays have not yet been added to this page.

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.

Live TransitSatellite experience

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Learning

Questions to explore

  • Why do low-orbiting stations circle Earth many times per day?
  • How do crews receive power, supplies, and communications in orbit?

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 20, 2026, 2:45 AM UTC

Story review

1970-01-01T00:00:00.000Z