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: 4 hours ago
TLE from 4 hours ago
0 RAPTOR3
1 58958U 24028D 26078.31318729 -.00000056 00000-0 24205-4 0 9997
2 58958 39.9904 96.2822 0010701 97.6021 262.5941 13.70481597104733Epoch: 2026-03-19T07:30Z
TLE epoch observation values (Epoch: 2026-03-19T07:30:59.381Z)
Latitude
-0.00005°
Longitude
166.67033°
Altitude
998.349 km
Speed
7.354 km/s
True Right ascension
06h 25m 07s
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
16:34:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,008.015 km
Perigee altitude
992.224 km
Semi-major axis
7,378.256 km
Eccentricity
0.00107
Inclination
39.9904°
RAAN
96.2822°
Arg. of periapsis
97.6021°
True anomaly
262.47252°
Mean anomaly
262.5941°
Eccentric anomaly
262.53331°
Mean motion
3.42462 °/min
Orbital period
105.12 mins
BSTAR
0.000024205
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-20 02:54:44.683Z | 174.772° S | 2026-03-20 02:57:44.683Z | 145.308° SSE | 17.03° | 2026-03-20 03:01:44.683Z | 104.908° ESE |
| 11 mins | 2026-03-20 04:43:44.683Z | 225.027° WSW | 2026-03-20 04:48:44.683Z | 146.62° SSE | 38.285° | 2026-03-20 04:54:44.683Z | 81.411° E |
| 11 mins | 2026-03-20 06:34:44.683Z | 262.076° W | 2026-03-20 06:39:44.683Z | 97.272° ESE | 44.764° | 2026-03-20 06:45:44.683Z | 85.36° E |
| 11 mins | 2026-03-20 08:25:44.683Z | 277.099° WNW | 2026-03-20 08:30:44.683Z | 181.172° SSW | 44.517° | 2026-03-20 08:36:44.683Z | 107.561° ESE |
| 10 mins | 2026-03-20 10:16:44.683Z | 269.858° W | 2026-03-20 10:21:44.683Z | 203.304° SW | 31.634° | 2026-03-20 10:26:44.683Z | 147.063° SSE |
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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