CZ-7 R/B, 69050

Orbit data source: Space-Track

CZ-7 R/B, 69050 is space debris in LEO originally from a Chinese launch on Mon, 11 May 2026 UTC launched from the Wenchang Satellite Launch Center (WSC). 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
69050, 2026-102B
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-05-11 (23 hours ago)
Launch vehicle
Unknown
Launch site
Wenchang Satellite Launch Center (WSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 CZ-7 R/B
1 69050U 26102B   26131.67280541  .00263037  75394-5  21344-3 0  9998
2 69050  41.4930 183.9016 0093059 176.6838 183.4652 16.04320735   107
Epoch: 2026-05-11T16:08Z
TLE epoch observation values (Epoch: 2026-05-11T16:08:50.387Z)
Latitude
0.00001°
Longitude
72.2335°
Altitude
323.739 km
Speed
7.68 km/s
True Right ascension
12h 15m 36s
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
19:01:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
326.557 km
Perigee altitude
202.921 km
Semi-major axis
6,642.876 km
Eccentricity
0.00931
Inclination
41.493°
RAAN
183.9016°
Arg. of periapsis
176.6838°
True anomaly
183.40149°
Mean anomaly
183.4652°
Eccentric anomaly
183.43327°
Mean motion
4.00875 °/min
Orbital period
89.8 mins
BSTAR
0.00021344
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Other satellites on launch #102 in the year 2026 (2026-05-11 UTC)

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