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: 13 hours ago
TLE from 13 hours ago
0 RAPTOR3
1 58958U 24028D 25259.21359181 -.00000046 00000-0 35543-4 0 9999
2 58958 39.9901 222.1013 0010768 118.2228 241.9606 13.70462863 79470Epoch: 2025-09-16T05:07Z
TLE epoch observation values (Epoch: 2025-09-16T05:07:34.332Z)
Latitude
-0.00006°
Longitude
149.80106°
Altitude
1,001.13 km
Speed
7.351 km/s
True Right ascension
14h 48m 24s
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
10:39:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,008.132 km
Perigee altitude
992.242 km
Semi-major axis
7,378.324 km
Eccentricity
0.00108
Inclination
39.9901°
RAAN
222.1013°
Arg. of periapsis
118.2228°
True anomaly
241.85176°
Mean anomaly
241.9606°
Eccentric anomaly
241.90617°
Mean motion
3.42457 °/min
Orbital period
105.12 mins
BSTAR
0.000035543
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-17 00:32:24.707Z | 213.378° SW | 2025-09-17 00:38:24.707Z | 142.948° SSE | 31.167° | 2025-09-17 00:43:24.707Z | 87.26° E |
| 11 mins | 2025-09-17 02:23:24.707Z | 251.218° W | 2025-09-17 02:28:24.707Z | 209.509° SW | 44.011° | 2025-09-17 02:34:24.707Z | 82.296° E |
| 11 mins | 2025-09-17 04:15:24.707Z | 274.406° WNW | 2025-09-17 04:20:24.707Z | 104.552° ESE | 44.661° | 2025-09-17 04:26:24.707Z | 97.344° ESE |
| 10 mins | 2025-09-17 06:06:24.707Z | 273.808° WNW | 2025-09-17 06:11:24.707Z | 191.715° SSW | 38.553° | 2025-09-17 06:16:24.707Z | 131.69° SE |
| 7 mins | 2025-09-17 07:58:24.707Z | 250.115° W | 2025-09-17 08:01:24.707Z | 218.54° SW | 17.591° | 2025-09-17 08:05:24.707Z | 179.633° 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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