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THEMIS E, 30798

Orbit data source: Space-Track

THEMIS E, 30798 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
30798, 2007-004E
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: 6 days ago

TLE from 6 days ago
0 THEMIS E
1 30798U 07004E   26169.54314664 -.00000327  00000-0  00000-0 0  9998
2 30798   6.3692  98.0709 8440072 215.6799 161.0349  0.88041867 65931
Epoch: 2026-06-18T13:02Z
TLE epoch observation values (Epoch: 2026-06-18T13:02:07.869Z)
Latitude
3.44631°
Longitude
28.19579°
Altitude
77,829.09 km
Speed
0.894 km/s
True Right ascension
08h 42m 03s
True Declination
3° 26' 40"
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
21:06:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
78,428.422 km
Perigee altitude
796.028 km
Semi-major axis
45,990.362 km
Eccentricity
0.84401
Inclination
6.3692°
RAAN
98.0709°
Arg. of periapsis
215.6799°
True anomaly
176.99385°
Mean anomaly
161.0349°
Eccentric anomaly
169.68985°
Mean motion
0.22006 °/min
Orbital period
1,635.91 mins
BSTAR
0
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