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THEMIS A, 30580

Orbit data source: Space-Track

THEMIS A, 30580 is a payload satellite owned by GSFC (US) in HEO that was launched on Sat, 17 Feb 2007 UTC via a DELTA 7925-10C 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
30580, 2007-004A
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Swales
Mission
Operational Civil Science
Bus & Motor
ATK-A100, Unknown motor
Mass
125 kg wet, 76 kg dry
Launch date (UTC)
2007-02-17 (19 years ago)
Launch vehicle
DELTA 7925-10C
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 6 Rod, 24.5 m
Radar Cross Section
0.720 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 THEMIS A
1 30580U 07004A   26070.91934435 -.00000206  00000-0 -29202-1 0  9996
2 30580   6.8693 119.2912 8401814 179.1358 185.6462  0.87846438 40425
Epoch: 2026-03-11T22:03Z
TLE epoch observation values (Epoch: 2026-03-11T22:03:51.351Z)
Latitude
0.00032°
Longitude
-21.17448°
Altitude
78,295.231 km
Speed
0.871 km/s
True Right ascension
07h 57m 27s
True Declination
0° 00' 01"
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
02:19:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
78,377.51 km
Perigee altitude
982.838 km
Semi-major axis
46,058.311 km
Eccentricity
0.84018
Inclination
6.8693°
RAAN
119.2912°
Arg. of periapsis
179.1358°
True anomaly
180.90463°
Mean anomaly
185.6462°
Eccentric anomaly
183.06895°
Mean motion
0.21957 °/min
Orbital period
1,639.54 mins
BSTAR
-0.029202
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