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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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Identifier
58958, 2024-028D
Orbit
LEO
Country
Flag of USUS
Related 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)
2024-02-14 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 1.0 m
Radar Cross Section
0.945 m², Large (>1 m²)

Expand to show TLE details & history
Last 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 13.70486078114741
Epoch: 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
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:35:54
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)

Documentation

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