RAPTOR3, 58958
Orbit data source: Space-Track
RAPTOR3, 58958 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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58958 intel report (Beta)
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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: 7 hours ago
TLE from 7 hours ago
0 RAPTOR3
1 58958U 24028D 26258.25678876 -.00000050 00000-0 31670-4 0 9990
2 58958 39.9929 349.5422 0010278 51.8807 308.2865 13.70489137129427Epoch: 2026-09-15T06:09Z
TLE epoch observation values (Epoch: 2026-09-15T06:09:46.548Z)
Latitude
-0.00002°
Longitude
-97.12711°
Altitude
992.605 km
Speed
7.359 km/s
True Right ascension
23h 18m 10s
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
06:15:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,007.675 km
Perigee altitude
992.509 km
Semi-major axis
7,378.229 km
Eccentricity
0.00103
Inclination
39.9929°
RAAN
349.5422°
Arg. of periapsis
51.8807°
True anomaly
308.19398°
Mean anomaly
308.2865°
Eccentric anomaly
308.24025°
Mean motion
3.42464 °/min
Orbital period
105.12 mins
BSTAR
0.00003167
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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.RAPTOR3 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-15 13:37:28.258Z | 272.203° WNW | 2026-09-15 13:39:28.258Z | 162.683° S | 82.54° | 2026-09-15 13:45:28.258Z | 104.31° ESE |
| 10 mins | 2026-09-15 15:25:28.258Z | 271.336° WNW | 2026-09-15 15:30:28.258Z | 201.284° SSW | 42.422° | 2026-09-15 15:35:28.258Z | 142.839° SSE |
| 9 mins | 2026-09-16 08:34:28.258Z | 195.795° SSW | 2026-09-16 08:38:28.258Z | 149.745° SSE | 29.016° | 2026-09-16 08:43:28.258Z | 92.657° ESE |
| 11 mins | 2026-09-16 10:24:28.258Z | 241.897° WSW | 2026-09-16 10:29:28.258Z | 150.643° SSE | 69.809° | 2026-09-16 10:35:28.258Z | 80.796° E |
| 11 mins | 2026-09-16 12:15:28.258Z | 271.068° WNW | 2026-09-16 12:20:28.258Z | 17.098° NNE | 88.374° | 2026-09-16 12:26:28.258Z | 91.539° ESE |
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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