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EXPLORER 29 (GEOS 1), 1726

Orbit data source: Space-Track

EXPLORER 29 (GEOS 1), 1726 is a payload satellite owned by GSFC (US) in LEO that was launched on Sat, 06 Nov 1965 UTC via a THOR DELTA E 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
1726, 1965-089A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
ANNA, Unknown motor
Mass
176 kg wet, 176 kg dry
Launch date (UTC)
1965-11-06 (60 years ago)
Launch vehicle
THOR DELTA E
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 EXPLORER 29 (GEOS 1)
1 01726U 65089A   25293.88006679 -.00000034  00000-0  25572-3 0  9991
2 01726  59.3785 207.0433 0719352  64.7373   1.2325 11.97072509621015
Epoch: 2025-10-20T21:07Z
TLE epoch observation values (Epoch: 2025-10-20T21:07:17.770Z)
Latitude
52.04958°
Longitude
-90.32963°
Altitude
1,120.425 km
Speed
7.556 km/s
True Right ascension
17h 04m 16s
True Declination
51° 53' 27"
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
23:37:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,274.017 km
Perigee altitude
1,112.763 km
Semi-major axis
8,071.527 km
Eccentricity
0.07194
Inclination
59.3785°
RAAN
207.0433°
Arg. of periapsis
64.7373°
True anomaly
1.42724°
Mean anomaly
1.2325°
Eccentric anomaly
1.32802°
Mean motion
2.99302 °/min
Orbital period
120.28 mins
BSTAR
0.00025572
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