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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Identifier
62853, 2025-021B
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX
Mission
Spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~4,000 kg wet, ~4,000 kg dry
Launch date (UTC)
2025-01-30 (1 year ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
39.980 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 FALCON 9 R/B
1 62853U 25021B   26170.58840425 -.00000258  00000-0  11591-2 0  9991
2 62853  24.7308 259.4812 8254049 318.7282   2.8025  1.11107236  5615
Epoch: 2026-06-19T14:07Z
TLE epoch observation values (Epoch: 2026-06-19T14:07:18.127Z)
Latitude
0.00011°
Longitude
139.88202°
Altitude
1,374.109 km
Speed
9.628 km/s
True Right ascension
17h 18m 05s
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
07:18:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
65,508.856 km
Perigee altitude
497.662 km
Semi-major axis
39,381.396 km
Eccentricity
0.8254
Inclination
24.7308°
RAAN
259.4812°
Arg. of periapsis
318.7282°
True anomaly
46.70118°
Mean anomaly
2.8025°
Eccentric anomaly
15.20987°
Mean motion
0.27772 °/min
Orbital period
1,296.27 mins
BSTAR
0.0011591
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Other satellites on launch #21 in the year 2025 (2025-01-30 UTC)

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