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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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 (10 months 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: 10 hours ago

TLE from 10 hours ago

0 CZ-6A R/B
1 62803U 25016U   25340.57531343  .00000766  00000-0  17127-3 0  9998
2 62803  89.0084  99.5786 0102929 106.4912 254.7636 14.52364122 46036

Epoch: 2025-12-06T13:48Z

TLE epoch observation values (Epoch: 2025-12-06T13:48:27.080Z)

Latitude

0.00001°

Longitude

176.86468°

Altitude

740.934 km

Speed

7.474 km/s

True Right ascension

06h 38m 18s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

21:40:34

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

787.849 km

Perigee altitude

641.835 km

Semi-major axis

7,092.979 km

Eccentricity

0.01029

Inclination

89.0084°

RAAN

99.5786°

Arg. of periapsis

106.4912°

True anomaly

253.62949°

Mean anomaly

254.7636°

Eccentric anomaly

254.19615°

Mean motion

3.63329 °/min

Orbital period

99.08 mins

BSTAR

0.00017127

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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.
8 mins	2025-12-07 08:07:02.133Z	154.685° SSE	2025-12-07 08:11:02.133Z	75.711° E	36.295°	2025-12-07 08:15:02.133Z	12.065° NNE
7 mins	2025-12-07 20:09:02.133Z	11.795° NNE	2025-12-07 20:12:02.133Z	66.687° ENE	40.697°	2025-12-07 20:16:02.133Z	167.922° 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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Check out CZ-6A R/B, 62803 on other resources

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View CZ-6A R/B, 62803 on Keep Track

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

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

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CZ-6A R/B, 62803

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2025-12-06T13:48:27.080Z)

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: 10 hours ago