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RAPTOR1, 58957

Orbit data source: Space-Track

RAPTOR1, 58957 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
58957, 2024-028C
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: 14 hours ago

TLE from 14 hours ago
0 RAPTOR1
1 58957U 24028C   25259.24636327 -.00000030  00000-0  53730-4 0  9992
2 58957  39.9892 222.2756 0011213 116.3538 243.8361 13.70286487 79477
Epoch: 2025-09-16T05:54Z
TLE epoch observation values (Epoch: 2025-09-16T05:54:45.786Z)
Latitude
-0.00001°
Longitude
138.1454°
Altitude
1,001.678 km
Speed
7.351 km/s
True Right ascension
14h 49m 06s
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
12:42:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,009.094 km
Perigee altitude
992.546 km
Semi-major axis
7,378.957 km
Eccentricity
0.00112
Inclination
39.9892°
RAAN
222.2756°
Arg. of periapsis
116.3538°
True anomaly
243.72085°
Mean anomaly
243.8361°
Eccentric anomaly
243.77847°
Mean motion
3.42413 °/min
Orbital period
105.14 mins
BSTAR
0.00005373
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Other satellites on launch #28 in the year 2024 (2024-02-14 UTC)

Documentation

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