RAPTOR2, 58959
Orbit data source: Space-Track
RAPTOR2, 58959 is a payload satellite owned by SDA (US) in LEO that was launched on Wed, 14 Feb 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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58959 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
L3Harris SIS
Mission
Operational Defense Early Warn
Bus & Motor
TPL0-L3H, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.0 m
Radar Cross Section
0.945 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 RAPTOR2
1 58959U 24028E 25259.26304837 -.00000037 00000-0 45201-4 0 9995
2 58959 39.9897 221.6125 0010973 120.0499 240.1338 13.70526048 79482Epoch: 2025-09-16T06:18Z
TLE epoch observation values (Epoch: 2025-09-16T06:18:47.379Z)
Latitude
0.00006°
Longitude
131.45929°
Altitude
1,001.2 km
Speed
7.351 km/s
True Right ascension
14h 46m 27s
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
12:42:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,008.056 km
Perigee altitude
991.864 km
Semi-major axis
7,378.097 km
Eccentricity
0.0011
Inclination
39.9897°
RAAN
221.6125°
Arg. of periapsis
120.0499°
True anomaly
240.02483°
Mean anomaly
240.1338°
Eccentric anomaly
240.07931°
Mean motion
3.42473 °/min
Orbital period
105.12 mins
BSTAR
0.000045201
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Other satellites on launch #28 in the year 2024 (2024-02-14 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.RAPTOR2 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-16 23:57:50.220Z | 196.379° SSW | 2025-09-17 00:02:50.220Z | 141.982° SSE | 24.262° | 2025-09-17 00:07:50.220Z | 91.094° ESE |
| 11 mins | 2025-09-17 01:47:50.220Z | 239.959° WSW | 2025-09-17 01:52:50.220Z | 179.364° S | 42.331° | 2025-09-17 01:58:50.220Z | 81.733° E |
| 12 mins | 2025-09-17 03:38:50.220Z | 269.381° W | 2025-09-17 03:43:50.220Z | 275.095° WNW | 44.47° | 2025-09-17 03:50:50.220Z | 90.578° ESE |
| 11 mins | 2025-09-17 05:30:50.220Z | 276.161° WNW | 2025-09-17 05:35:50.220Z | 175.566° S | 42.316° | 2025-09-17 05:41:50.220Z | 117.802° SE |
| 9 mins | 2025-09-17 07:21:50.220Z | 262.451° W | 2025-09-17 07:25:50.220Z | 216.656° SW | 24.528° | 2025-09-17 07:30:50.220Z | 162.479° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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