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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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: 22 hours ago
TLE from 22 hours ago
0 RAPTOR3
1 58958U 24028D 25291.13599678 -.00000025 00000-0 58767-4 0 9993
2 58958 39.9911 75.4373 0012361 298.1930 61.7568 13.70466327 83859Epoch: 2025-10-18T03:15Z
TLE epoch observation values (Epoch: 2025-10-18T03:15:50.121Z)
Latitude
-0.00002°
Longitude
-0.39291°
Altitude
993.073 km
Speed
7.359 km/s
True Right ascension
05h 01m 44s
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
19:52:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,009.294 km
Perigee altitude
991.054 km
Semi-major axis
7,378.311 km
Eccentricity
0.00124
Inclination
39.9911°
RAAN
75.4373°
Arg. of periapsis
298.193°
True anomaly
61.88167°
Mean anomaly
61.7568°
Eccentric anomaly
61.81923°
Mean motion
3.42458 °/min
Orbital period
105.12 mins
BSTAR
0.000058767
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-19 10:54:19.657Z | 157.237° SSE | 2025-10-19 10:56:19.657Z | 138.977° SSE | 12.204° | 2025-10-19 10:58:19.657Z | 120.374° SE |
| 10 mins | 2025-10-19 12:42:19.657Z | 212.15° SW | 2025-10-19 12:46:19.657Z | 158.757° S | 33.91° | 2025-10-19 12:52:19.657Z | 84.68° E |
| 11 mins | 2025-10-19 14:32:19.657Z | 255.094° W | 2025-10-19 14:37:19.657Z | 197.411° SSW | 44.716° | 2025-10-19 14:43:19.657Z | 82.921° E |
| 12 mins | 2025-10-19 16:23:19.657Z | 275.775° WNW | 2025-10-19 16:28:19.657Z | 257.579° W | 44.541° | 2025-10-19 16:35:19.657Z | 100.558° ESE |
| 10 mins | 2025-10-19 18:15:19.657Z | 271.041° WNW | 2025-10-19 18:19:19.657Z | 216.032° SW | 36.613° | 2025-10-19 18:25:19.657Z | 136.048° SSE |
| 6 mins | 2025-10-19 20:07:19.657Z | 246.436° WSW | 2025-10-19 20:10:19.657Z | 216.686° SW | 15.135° | 2025-10-19 20:13:19.657Z | 188.85° SSW |
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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