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). Payloads include a variety of satellites, spacecraft, and rockets 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 | LEO |
| Last TLE update | 21 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Pan, 2 m |
| Radar Cross Section | 0.945 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 21 hours ago
0 RAPTOR3
1 58958U 24028D 25077.22542188 .00000032 00000-0 12267-3 0 9990
2 58958 39.9929 338.1946 0010437 150.4005 209.7334 13.70447343 54500Epoch: 2025-03-18T05:24Z
Definitive object data (Epoch: 2025-03-18T05:24:36.45Z)
| Latitude | -0° |
| Longitude | 81.01177° |
| Altitude | 1,004.133 km |
| Speed | 7.348 km/s |
| True Right ascension | 22h 32m 46s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 38.85178° |
| Longitude | 149.71274° |
| Altitude | 998.495 km |
| Speed | 7.358 km/s |
| Apparent Right ascension | 23h 48m 24s |
| Apparent Declination | 5° 11' 51" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 07:33:32 |
| Azimuth | 291.538° WNW |
| Elevation | -16.265° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,007.943 km |
| Perigee altitude | 992.541 km |
| Semi-major axis | 7,378.379 km |
| Eccentricity | 0.0010437 |
| Inclination | 39.9929° |
| RAAN | 338.1946° |
| Arg. of periapsis | 150.4005° |
| True anomaly | 209.67415° |
| Mean anomaly | 209.7334° |
| Eccentric anomaly | 209.70377° |
| Mean motion | 3.42454 °/min |
| BSTAR | 0.00012267 |
| Orbital period | 105.12 mins |
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Other satellites on launch #28 in the year 2024 (2024-02-14 UTC)
| HBTSS-SV2, 58955 |
| RAPTOR4, 58956 |
| RAPTOR1, 58957 |
| RAPTOR2, 58959 |
| HBTSS-SV1, 58960 |
RAPTOR3 Visibility forecast
Observer location: undefined°, undefined
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 | 2025-03-19 02:56:22.492Z | 269.446° W | 2025-03-19 03:01:22.492Z | 214.3° SW | 26.968° | 2025-03-19 03:06:22.492Z | 157.878° S |
| 10 mins | 2025-03-19 20:05:22.492Z | 211.487° SW | 2025-03-19 20:10:22.492Z | 142.616° SSE | 32.714° | 2025-03-19 20:15:22.492Z | 86.409° E |
| 12 mins | 2025-03-19 21:55:22.492Z | 253.526° W | 2025-03-19 22:00:22.492Z | 218.56° SW | 44.183° | 2025-03-19 22:07:22.492Z | 82.237° E |
| 11 mins | 2025-03-19 23:47:22.492Z | 275.161° WNW | 2025-03-19 23:52:22.492Z | 114.946° SE | 44.7° | 2025-03-19 23:58:22.492Z | 99.122° ESE |
| 10 mins | 2025-03-20 01:38:22.492Z | 273.052° WNW | 2025-03-20 01:43:22.492Z | 194.082° SSW | 37.404° | 2025-03-20 01:48:22.492Z | 134.606° SE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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