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RAPTOR4, 58956

Orbit data source: Space-Track

RAPTOR4, 58956 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
58956, 2024-028B
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: 1 week ago

TLE from 1 week ago
0 RAPTOR4
1 58956U 24028B   26152.24402784 -.00000065  00000-0  14093-4 0  9999
2 58956  39.9892 117.6832 0014354 151.6789 208.4740 13.70381991114864
Epoch: 2026-06-01T05:51Z
TLE epoch observation values (Epoch: 2026-06-01T05:51:24.005Z)
Latitude
-0.00002°
Longitude
140.09902°
Altitude
1,006.99 km
Speed
7.345 km/s
True Right ascension
07h 50m 43s
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
15:54:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,011.068 km
Perigee altitude
989.886 km
Semi-major axis
7,378.614 km
Eccentricity
0.00144
Inclination
39.9892°
RAAN
117.6832°
Arg. of periapsis
151.6789°
True anomaly
208.3957°
Mean anomaly
208.474°
Eccentric anomaly
208.43484°
Mean motion
3.42437 °/min
Orbital period
105.13 mins
BSTAR
0.000014093
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Other satellites on launch #28 in the year 2024 (2024-02-14 UTC)

Documentation

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