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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: 7 hours ago

TLE from 7 hours ago
0 EXPLORER 29 (GEOS 1)
1 01726U 65089A   26070.88513851 -.00000046  00000-0  17782-3 0  9997
2 01726  59.3776 247.7769 0717893 157.0808 327.6265 11.97075072638019
Epoch: 2026-03-11T21:14Z
TLE epoch observation values (Epoch: 2026-03-11T21:14:35.967Z)
Latitude
48.33844°
Longitude
-101.858°
Altitude
1,223.747 km
Speed
7.458 km/s
True Right ascension
01h 45m 20s
True Declination
48° 10' 41"
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
08:45:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,272.827 km
Perigee altitude
1,113.93 km
Semi-major axis
8,071.515 km
Eccentricity
0.07179
Inclination
59.3776°
RAAN
247.7769°
Arg. of periapsis
157.0808°
True anomaly
322.86739°
Mean anomaly
327.6265°
Eccentric anomaly
325.28398°
Mean motion
2.99303 °/min
Orbital period
120.28 mins
BSTAR
0.00017782
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