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GEOTAIL, 22049

Orbit data source: Space-Track

GEOTAIL, 22049 is a payload satellite owned by ISAS (JP) in HEO that was launched on Fri, 24 Jul 1992 UTC via a DELTA 6925 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
22049, 1992-044A
Orbit
HEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
NEC
Mission
Non-operational Civil Science
Bus & Motor
GEOTAIL, Unknown motor
Mass
1,009 kg wet, 640 kg dry
Launch date (UTC)
1992-07-24 (34 years ago)
Launch vehicle
DELTA 6925
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Ant, 1.1 m
Radar Cross Section
15.169 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: in 2 days

TLE from in 2 days
0 GEOTAIL
1 22049U 92044A   26157.56173069 -.00001559  00000-0  00000-0 0  9995
2 22049  45.3349 344.8330 5742418 280.6441 357.9112  0.19182450 15732
Epoch: 2026-06-06T13:28Z
TLE epoch observation values (Epoch: 2026-06-06T13:28:53.531Z)
Latitude
-45.15298°
Longitude
162.81907°
Altitude
46,645.929 km
Speed
3.45 km/s
True Right ascension
17h 20m 04s
True Declination
-45° 07' 48"
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
21:46:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
193,548.818 km
Perigee altitude
47,692.68 km
Semi-major axis
126,998.886 km
Eccentricity
0.57424
Inclination
45.3349°
RAAN
344.833°
Arg. of periapsis
280.6441°
True anomaly
350.59706°
Mean anomaly
357.9112°
Eccentric anomaly
355.10197°
Mean motion
0.04796 °/min
Orbital period
7,506.88 mins
BSTAR
0
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Other satellites on launch #44 in the year 1992 (1992-07-24 UTC)

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