FALCON 9 R/B, 62878 (Decayed)
Orbit data source: Space-Track
FALCON 9 R/B, 62878 was space debris in LEO originally from a launch on Sat, 01 Feb 2025 UTC launched from the Air Force Western Test Range (AFWTR). 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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62878 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX
Mission
Decayed spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~3,000 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 7.8 m
Radar Cross Section
39.980 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 FALCON 9 R/B
1 62878U 25022Y 25050.09289105 .10554311 13066-4 11008-3 0 9991
2 62878 53.1436 118.6486 0031063 5.7660 67.2814 16.47531719 2741Epoch: 2025-02-19T02:13Z
TLE epoch observation values (Epoch: 2025-02-19T02:13:45.786Z)
Latitude
50.21461°
Longitude
-0.57115°
Altitude
143.888 km
Speed
7.831 km/s
True Right ascension
12h 08m 37s
True Declination
50° 01' 46"
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
02:14:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
166.381 km
Perigee altitude
125.849 km
Semi-major axis
6,524.252 km
Eccentricity
0.00311
Inclination
53.1436°
RAAN
118.6486°
Arg. of periapsis
5.766°
True anomaly
67.61023°
Mean anomaly
67.2814°
Eccentric anomaly
67.44577°
Mean motion
4.11858 °/min
Orbital period
87.41 mins
BSTAR
0.00011008
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Other satellites on launch #22 in the year 2025 (2025-02-01 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.FALCON 9 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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