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 (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: 8 hours ago

TLE from 8 hours ago

0 CZ-6A R/B
1 62803U 25016U   26035.79103750  .00000434  00000-0  96217-4 0  9991
2 62803  89.0038  92.4358 0098081 260.5899  98.4211 14.52413880 54779

Epoch: 2026-02-04T18:59Z

TLE epoch observation values (Epoch: 2026-02-04T18:59:05.639Z)

Latitude

-0.00005°

Longitude

32.70975°

Altitude

731.736 km

Speed

7.483 km/s

True Right ascension

06h 09m 44s

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

05:00:13

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

784.247 km

Perigee altitude

645.113 km

Semi-major axis

7,092.817 km

Eccentricity

0.00981

Inclination

89.0038°

RAAN

92.4358°

Arg. of periapsis

260.5899°

True anomaly

99.53085°

Mean anomaly

98.4211°

Eccentric anomaly

98.97618°

Mean motion

3.63342 °/min

Orbital period

99.08 mins

BSTAR

0.000096217

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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	2026-02-05 03:22:34.805Z	138.779° SSE	2026-02-05 03:26:34.805Z	77.937° E	28.109°	2026-02-05 03:30:34.805Z	21.507° NNE
7 mins	2026-02-05 05:02:34.805Z	230.015° WSW	2026-02-05 05:05:34.805Z	277.246° WNW	24.685°	2026-02-05 05:09:34.805Z	332.534° NNW
7 mins	2026-02-05 15:25:34.805Z	25.718° NE	2026-02-05 15:28:34.805Z	81.4° E	32.981°	2026-02-05 15:32:34.805Z	151.628° SSE
5 mins	2026-02-05 17:05:34.805Z	312.404° NW	2026-02-05 17:07:34.805Z	281.889° WNW	19.753°	2026-02-05 17:10:34.805Z	240.492° WSW

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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: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-02-04T18:59:05.639Z)

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: 8 hours ago