Showing default

OPS 6582 (TRANSIT 5E-5), 959

Orbit data source: Space-Track

OPS 6582 (TRANSIT 5E-5), 959 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Sun, 13 Dec 1964 UTC via a THOR ABLESTAR 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
959, 1964-083C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
77 kg wet, 77 kg dry
Launch date (UTC)
1964-12-13 (61 years ago)
Launch vehicle
THOR ABLESTAR
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 OPS 6582 (TRANSIT 5E-5)
1 00959U 64083C   26076.84004461  .00000170  00000-0  20577-3 0  9994
2 00959  90.0117 187.2197 0041423 210.3120 264.2083 13.62465804 37779
Epoch: 2026-03-17T20:09Z
TLE epoch observation values (Epoch: 2026-03-17T20:09:39.854Z)
Latitude
66.03181°
Longitude
-110.58258°
Altitude
1,041.467 km
Speed
7.336 km/s
True Right ascension
00h 28m 59s
True Declination
65° 54' 32"
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
15:26:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,054.437 km
Perigee altitude
993.115 km
Semi-major axis
7,401.913 km
Eccentricity
0.00414
Inclination
90.0117°
RAAN
187.2197°
Arg. of periapsis
210.312°
True anomaly
263.7363°
Mean anomaly
264.2083°
Eccentric anomaly
263.97228°
Mean motion
3.40822 °/min
Orbital period
105.63 mins
BSTAR
0.00020577
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|