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: 2 weeks ago
TLE from 2 weeks ago
0 RAPTOR3
1 58958U 24028D 26151.26734621 -.00000038 00000-0 44523-4 0 9991
2 58958 39.9896 121.0984 0011113 161.8137 198.3009 13.70486078114741Epoch: 2026-05-31T06:24Z
TLE epoch observation values (Epoch: 2026-05-31T06:24:58.712Z)
Latitude
0.00001°
Longitude
136.0823°
Altitude
1,005.089 km
Speed
7.347 km/s
True Right ascension
08h 04m 23s
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
15:50:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,008.303 km
Perigee altitude
991.904 km
Semi-major axis
7,378.24 km
Eccentricity
0.00111
Inclination
39.9896°
RAAN
121.0984°
Arg. of periapsis
161.8137°
True anomaly
198.26097°
Mean anomaly
198.3009°
Eccentric anomaly
198.28093°
Mean motion
3.42463 °/min
Orbital period
105.12 mins
BSTAR
0.000044523
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-11 20:42:18.750Z | 205.394° SW | 2026-06-11 20:47:18.750Z | 147.277° SSE | 28.997° | 2026-06-11 20:52:18.750Z | 89.949° E |
| 11 mins | 2026-06-11 22:33:18.750Z | 246.386° WSW | 2026-06-11 22:38:18.750Z | 136.951° SSE | 43.75° | 2026-06-11 22:44:18.750Z | 81.27° E |
| 11 mins | 2026-06-12 00:24:18.750Z | 272.932° WNW | 2026-06-12 00:29:18.750Z | 92.24° ESE | 44.96° | 2026-06-12 00:35:18.750Z | 94.677° ESE |
| 11 mins | 2026-06-12 02:15:18.750Z | 275.792° WNW | 2026-06-12 02:20:18.750Z | 199.724° SSW | 40.524° | 2026-06-12 02:26:18.750Z | 125.639° SE |
| 8 mins | 2026-06-12 04:07:18.750Z | 254.311° W | 2026-06-12 04:10:18.750Z | 222.059° SW | 20.126° | 2026-06-12 04:15:18.750Z | 171.673° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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