CZ-7 R/B, 69050 (Decayed)
Orbit data source: Space-Track
CZ-7 R/B, 69050 was space debris in LEO originally from a 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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69050 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-7 STAGE 2, Unknown motor
Mass
6,000 kg wet, 6,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 weeks ago
TLE from 4 weeks ago
0 CZ-7 R/B
1 69050U 26102B 26142.16904703 .12161917 82861-5 12633-3 0 9992
2 69050 41.4904 114.5024 0021849 260.8309 99.0090 16.48718798 1808Epoch: 2026-05-22T04:03Z
TLE epoch observation values (Epoch: 2026-05-22T04:03:25.663Z)
Latitude
0.00001°
Longitude
173.84173°
Altitude
144.56 km
Speed
7.82 km/s
True Right ascension
07h 38m 00s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:09:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
159.276 km
Perigee altitude
130.771 km
Semi-major axis
6,523.161 km
Eccentricity
0.00218
Inclination
41.4904°
RAAN
114.5024°
Arg. of periapsis
260.8309°
True anomaly
99.25618°
Mean anomaly
99.009°
Eccentric anomaly
99.1326°
Mean motion
4.11961 °/min
Orbital period
87.39 mins
BSTAR
0.00012633
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Other satellites on launch #102 in the year 2026 (2026-05-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-7 R/B Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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