Showing default

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.

Loading next visibility...
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 (61 years ago)
Launch vehicle
THOR DELTA E
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
OCT CYL + DOME + ANT, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 EXPLORER 29 (GEOS 1)
1 01726U 65089A   26279.12245071 -.00000082  00000-0 -56304-4 0  9996
2 01726  59.3814 139.7215 0711207 293.7796 240.6874 11.97077756662945
Epoch: 2026-10-06T02:56Z
TLE epoch observation values (Epoch: 2026-10-06T02:56:19.741Z)
Latitude
10.56319°
Longitude
-105.45951°
Altitude
2,005.024 km
Speed
6.764 km/s
True Right ascension
20h 53m 39s
True Declination
10° 30' 38"
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
11:18:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,267.417 km
Perigee altitude
1,119.315 km
Semi-major axis
8,071.503 km
Eccentricity
0.07112
Inclination
59.3814°
RAAN
139.7215°
Arg. of periapsis
293.7796°
True anomaly
233.89378°
Mean anomaly
240.6874°
Eccentric anomaly
237.25986°
Mean motion
2.99303 °/min
Orbital period
120.28 mins
BSTAR
-0.000056304
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|