CZ-6A R/B, 62803

Orbit data source: Space-Track

CZ-6A R/B, 62803 is space debris in LEO originally from a launch on Thu, 23 Jan 2025 UTC launched from the Taiyaun Space Center, China (TSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Iframe URL

https://www.satcat.com/sats-embedded/62803?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62803, 2025-016U

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-6A STAGE 2, YF-115

Mass

~6,000 kg wet, ~6,000 kg dry

Launch date (UTC)

2025-01-23 (1 year ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 4.4 m

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago

0 CZ-6A R/B
1 62803U 25016U   26092.28550724  .00000585  00000-0  12957-3 0  9990
2 62803  88.9998  85.6857 0102803  68.0709 293.1389 14.52450613 62975

Epoch: 2026-04-02T06:51Z

TLE epoch observation values (Epoch: 2026-04-02T06:51:07.825Z)

Latitude

0.00001°

Longitude

152.26692°

Altitude

692.722 km

Speed

7.525 km/s

True Right ascension

05h 42m 44s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

21:24:09

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

787.475 km

Perigee altitude

641.645 km

Semi-major axis

7,092.697 km

Eccentricity

0.01028

Inclination

88.9998°

RAAN

85.6857°

Arg. of periapsis

68.0709°

True anomaly

292.0502°

Mean anomaly

293.1389°

Eccentric anomaly

292.59509°

Mean motion

3.63351 °/min

Orbital period

99.08 mins

BSTAR

0.00012957

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Other satellites on launch #16 in the year 2025 (2025-01-23 UTC)

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CZ-6A R/B Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
7 mins	2026-04-02 23:30:38.375Z	152.056° SSE	2026-04-02 23:33:38.375Z	102.691° ESE	34.314°	2026-04-02 23:37:38.375Z	15.703° NNE
7 mins	2026-04-03 11:32:38.375Z	14.53° NNE	2026-04-03 11:35:38.375Z	90.323° ESE	41.059°	2026-04-03 11:39:38.375Z	167.764° S

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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View CZ-6A R/B, 62803 on Celestrak

View CZ-6A R/B, 62803 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CZ-6A R/B, 62803

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-04-02T06:51:07.825Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #16 in the year 2025 (2025-01-23 UTC)

CZ-6A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A R/B, 62803 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago