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EXPLORER 7, 22

Orbit data source: Space-Track

EXPLORER 7, 22 is a payload satellite owned by GSFC (US) in LEO that was launched on Tue, 13 Oct 1959 UTC via a JUNO II 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
22, 1959-009A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ABMA
Mission
Spacecraft
Bus & Motor
S-1, Unknown motor
Mass
41 kg wet, 41 kg dry
Launch date (UTC)
1959-10-13 (66 years ago)
Launch vehicle
JUNO II
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 EXPLORER 7
1 00022U 59009A   26019.28016479  .00015350  00000-0  56226-3 0  9990
2 00022  50.2394 114.5850 0085192 245.5798 113.6255 15.24774575777593
Epoch: 2026-01-19T06:43Z
TLE epoch observation values (Epoch: 2026-01-19T06:43:26.237Z)
Latitude
0.00001°
Longitude
-104.95296°
Altitude
515.911 km
Speed
7.594 km/s
True Right ascension
07h 38m 20s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
18:00:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.725 km
Perigee altitude
433.665 km
Semi-major axis
6,870.332 km
Eccentricity
0.00852
Inclination
50.2394°
RAAN
114.585°
Arg. of periapsis
245.5798°
True anomaly
114.51607°
Mean anomaly
113.6255°
Eccentric anomaly
114.07117°
Mean motion
3.81133 °/min
Orbital period
94.46 mins
BSTAR
0.00056226
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Other satellites on launch #9 in the year 1959 (1959-10-13 UTC)

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