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Tiangong Space Station

Tiangong is China's modular space station and a major step in the country's long-duration human-spaceflight program. Built around the Tianhe core module and expanded with Wentian and Mengtian laboratory modules, it supports crews, experiments and repeated cargo and crew missions in low Earth orbit.

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Object identity

NORAD ID
48274
COSPAR ID
2021-035A
Operator
China Manned Space Agency
Country
China
Launch date
April 29, 2021

Immediate discovery

Why this satellite matters

Tiangong is particularly useful for comparing independent space-station architectures: different launch vehicles, docking systems and mission cadence, but the same orbital mechanics govern every module once in orbit.

Understanding the mission

Science and engineering ideas

Tiangong is particularly useful for comparing independent space-station architectures: different launch vehicles, docking systems and mission cadence, but the same orbital mechanics govern every module once in orbit.

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.

  • Tiangong is particularly useful for comparing independent space-station architectures: different launch vehicles, docking systems and mission cadence, but the same orbital mechanics govern every module once in orbit.

Design

Engineering

Tiangong is particularly useful for comparing independent space-station architectures: different launch vehicles, docking systems and mission cadence, but the same orbital mechanics govern every module once in orbit.

Real orbital values

The mathematics

The current two-line element set reports approximately 15.6011 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

394 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

Tiangong assembly began with Tianhe's launch on 29 April 2021 aboard a Long March 5B from Wenchang. Wentian and Mengtian followed in 2022.

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

See Tiangong Space Station moving now

Open the live tracker to view its current calculated position, trajectory, orbital information, visibility tools, and Save and Share controls.

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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, 2:05 AM UTC

Story review

1970-01-01T00:00:00.000Z