Showing default

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.

Loading next visibility...
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: 10 hours ago

TLE from 10 hours ago
0 RAPTOR3
1 58958U 24028D   25352.13825493 -.00000012  00000-0  73769-4 0  9993
2 58958  39.9889 155.1754 0012439 290.1134  69.8274 13.70473777 92227
Epoch: 2025-12-18T03:19Z
TLE epoch observation values (Epoch: 2025-12-18T03:19:05.225Z)
Latitude
-0.00002°
Longitude
18.40554°
Altitude
994.198 km
Speed
7.358 km/s
True Right ascension
10h 20m 42s
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
12:28:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,009.326 km
Perigee altitude
990.97 km
Semi-major axis
7,378.285 km
Eccentricity
0.00124
Inclination
39.9889°
RAAN
155.1754°
Arg. of periapsis
290.1134°
True anomaly
69.96127°
Mean anomaly
69.8274°
Eccentric anomaly
69.89433°
Mean motion
3.4246 °/min
Orbital period
105.12 mins
BSTAR
0.000073769
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #28 in the year 2024 (2024-02-14 UTC)

Documentation

Showing up to 5 results
|