CZ-4C R/B, 49010

Orbit data source: Space-Track

CZ-4C R/B, 49010 is space debris in SSO originally from a launch on Sun, 04 Jul 2021 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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/49010?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

49010, 2021-062C

Orbit

SSO

Last TLE update

4 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

~1,000 kg wet, ~1,000 kg dry

Launch date (UTC)

2021-07-04 (4 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 2.9 m

Radar Cross Section

7.676 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 4 hours ago

0 CZ-4C R/B
1 49010U 21062C   25197.20904141  .00000189  00000-0  48973-4 0  9993
2 49010  98.5533 272.8099 0131676 236.4743 122.3820 14.56863668214197

Epoch: 2025-07-16T05:01Z

TLE epoch observation values (Epoch: 2025-07-16T05:01:01.177Z)

Latitude

0.00002°

Longitude

-96.7375°

Altitude

757.105 km

Speed

7.449 km/s

True Right ascension

18h 11m 14s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

53.87112°

Longitude

-108.41186°

Altitude

805.392 km

Speed

7.407 km/s

Apparent Right ascension

12h 47m 44s

Apparent Declination

21° 17' 59"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:11:25

Azimuth

309.831° NW

Elevation

-10.728°

Doppler factor

Orbital elements

Apogee altitude

793.628 km

Perigee altitude

607.213 km

Semi-major axis

7,078.557 km

Eccentricity

0.01317

Inclination

98.5533°

RAAN

272.8099°

Arg. of periapsis

236.4743°

True anomaly

Unknown

Mean anomaly

122.382°

Eccentric anomaly

Unknown

Mean motion

3.6444 °/min

Orbital period

98.78 mins

BSTAR

0.000048973

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Other satellites on launch #62 in the year 2021 (2021-07-04 UTC)

FENGYUN 3E, 49008

OBJECT B, 49009 (Decayed)

OBJECT D, 49024

OBJECT E, 49047

CZ-4C R/B Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-16 17:09:08.455Z	40.39° NE	2025-07-16 17:13:08.455Z	102.357° ESE	24.374°	2025-07-16 17:16:08.455Z	148.498° SSE
6 mins	2025-07-16 18:48:08.455Z	336.892° NNW	2025-07-16 18:50:08.455Z	300.902° NW	26.709°	2025-07-16 18:54:08.455Z	234.759° WSW
7 mins	2025-07-17 04:15:08.455Z	114.78° SE	2025-07-17 04:18:08.455Z	59.363° ENE	28.06°	2025-07-17 04:22:08.455Z	7.47° NNE
7 mins	2025-07-17 05:52:08.455Z	211.765° SW	2025-07-17 05:55:08.455Z	258.347° W	26.95°	2025-07-17 05:59:08.455Z	319.693° NNW

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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Authenticating...

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Check out CZ-4C R/B, 49010 on other resources

View CZ-4C R/B, 49010 on Heavens-Above

View CZ-4C R/B, 49010 on Keep Track

View CZ-4C R/B, 49010 on Celestrak

View CZ-4C R/B, 49010 on Gunter's Space Page

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