Showing default

EXPLORER 25 (INJUN-4), 932

Orbit data source: Space-Track

EXPLORER 25 (INJUN-4), 932 is a payload satellite owned by NASA LaRC (US) in LEO that was launched on Sat, 21 Nov 1964 UTC via an SCOUT X-4 launch vehicle from the Air Force Western Test Range (AFWTR). 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
932, 1964-076B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
BENDX/UIA
Mission
Spacecraft
Bus & Motor
BENDIX UTILITY, Unknown motor
Mass
41 kg wet, 41 kg dry
Launch date (UTC)
1964-11-21 (61 years ago)
Launch vehicle
SCOUT X-4
Launch site
Air Force Western Test Range (AFWTR)
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: 13 hours ago

TLE from 13 hours ago
0 EXPLORER 25 (INJUN-4)
1   932U 64076B   26038.25114995  .00001283  00000-0  45192-3 0  9990
2   932  81.3403 118.4939 1119283 202.9956 151.7079 12.67065644802672
Epoch: 2026-02-07T06:01Z
TLE epoch observation values (Epoch: 2026-02-07T06:01:39.355Z)
Latitude
-0.00005°
Longitude
-109.29744°
Altitude
2,181.744 km
Speed
6.471 km/s
True Right ascension
07h 53m 58s
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
20:44:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,260.843 km
Perigee altitude
521.619 km
Semi-major axis
7,769.368 km
Eccentricity
0.11193
Inclination
81.3403°
RAAN
118.4939°
Arg. of periapsis
202.9956°
True anomaly
157.10995°
Mean anomaly
151.7079°
Eccentric anomaly
154.47164°
Mean motion
3.16931 °/min
Orbital period
113.59 mins
BSTAR
0.00045192
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
|