FALCON 9 R/B, 62484
Orbit data source: Space-Track
FALCON 9 R/B, 62484 is space debris in HEO originally from a launch on Sat, 04 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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62484 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX
Mission
Spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~4,000 kg wet, ~4,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 5.4 m
Radar Cross Section
39.980 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 FALCON 9 R/B
1 62484U 25001B 26122.36904915 -.00000254 00000-0 10032-2 0 9992
2 62484 25.1359 219.8016 7899288 346.7661 1.0895 1.41763297 6854Epoch: 2026-05-02T08:51Z
TLE epoch observation values (Epoch: 2026-05-02T08:51:25.846Z)
Latitude
0.00016°
Longitude
-133.41589°
Altitude
692.154 km
Speed
10.042 km/s
True Right ascension
14h 38m 55s
True Declination
0° 00' 01"
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
08:31:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
53,543.361 km
Perigee altitude
654.423 km
Semi-major axis
33,477.029 km
Eccentricity
0.78993
Inclination
25.1359°
RAAN
219.8016°
Arg. of periapsis
346.7661°
True anomaly
14.98656°
Mean anomaly
1.0895°
Eccentric anomaly
5.16012°
Mean motion
0.35434 °/min
Orbital period
1,015.97 mins
BSTAR
0.0010032
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Other satellites on launch #1 in the year 2025 (2025-01-04 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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-05-07 07:31:43.473Z | 130.575° SE | 2026-05-07 07:35:43.473Z | 112.179° ESE | 11.866° | 2026-05-07 07:42:43.473Z | 94.94° ESE |
| 703 mins | 2026-05-07 11:27:43.473Z | 87.792° E | 2026-05-07 17:48:43.473Z | 166.614° S | 35.806° | 2026-05-07 23:10:43.473Z | 207.832° SW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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