CZ-4B R/B, 61938

Orbit data source: Space-Track

CZ-4B R/B, 61938 is space debris in SSO originally from a launch on Wed, 13 Nov 2024 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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Identifier
61938, 2024-208C
Orbit
SSO
Last TLE update
10 hours ago
Origin
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2024-11-13 (8 months ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.932 m
Radar Cross Section
14.536 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 10 hours ago
0 CZ-4B R/B
1 61938U 24208C   25196.93029324  .00004467  00000-0  15508-3 0  9991
2 61938  97.9866 221.3899 0143345 252.5266 106.0257 15.21101804 37022
Epoch: 2025-07-15T22:19Z
TLE epoch observation values (Epoch: 2025-07-15T22:19:37.335Z)
Latitude
-0.00009°
Longitude
-47.5334°
Altitude
534.124 km
Speed
7.58 km/s
True Right ascension
14h 45m 33s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
81.88165°
Longitude
-125.11987°
Altitude
610.104 km
Speed
7.509 km/s
Apparent Right ascension
08h 56m 42s
Apparent Declination
25° 41' 56"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
20:48:57
Azimuth
358.084° N
Elevation
-24.36°
Doppler factor
1
Orbital elements
Apogee altitude
598.093 km
Perigee altitude
400.918 km
Semi-major axis
6,877.642 km
Eccentricity
0.01433
Inclination
97.9866°
RAAN
221.3899°
Arg. of periapsis
252.5266°
True anomaly
Unknown
Mean anomaly
106.0257°
Eccentric anomaly
Unknown
Mean motion
3.80526 °/min
Orbital period
94.61 mins
BSTAR
0.00015508
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