FALCON 9 R/B, 62853
Orbit data source: Space-Track
FALCON 9 R/B, 62853 is space debris in HEO originally from a launch on Thu, 30 Jan 2025 UTC launched from the Air Force Eastern Test Range (AFETR). 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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62853 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FALCON 9 R/B
1 62853U 25021B 25240.28726488 .00001022 00000-0 28809-2 0 9996
2 62853 25.3495 309.5985 8309230 234.9878 18.8381 1.10774831 2338
Epoch: 2025-08-28T06:53Z
TLE epoch observation values (Epoch: 2025-08-28T06:53:39.685Z)
Latitude
0.00005°
Longitude
-130.43596°
Altitude
17,025.853 km
Speed
4.895 km/s
True Right ascension
20h 38m 55s
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
11:00:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
65,870.531 km
Perigee altitude
293.683 km
Semi-major axis
39,460.244 km
Eccentricity
0.83092
Inclination
25.3495°
RAAN
309.5985°
Arg. of periapsis
234.9878°
True anomaly
124.59131°
Mean anomaly
18.8381°
Eccentric anomaly
60.11647°
Mean motion
0.27689 °/min
Orbital period
1,300.17 mins
BSTAR
0.0028809
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Other satellites on launch #21 in the year 2025 (2025-01-30 UTC)
FALCON 9 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. |
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799 mins | 2025-08-30 01:44:50.156Z | 138.709° SSE | 2025-08-30 07:58:50.156Z | 187.506° SSW | 42.149° | 2025-08-30 15:03:50.156Z | 286.92° WNW |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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