Showing default

OPS 6582 (TRANSIT 5B-5), 965

Orbit data source: Space-Track

OPS 6582 (TRANSIT 5B-5), 965 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
965, 1964-083D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NAFI
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~54 kg wet, ~54 kg dry
Launch date (UTC)
1964-12-13 (62 years ago)
Launch vehicle
THOR ABLESTAR
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
OCT CYL + 4 PAN + ANT, 15.0 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 OPS 6582 (TRANSIT 5B-5)
1 00965U 64083D   26208.05938414  .00000062  00000-0  73057-4 0  9997
2 00965  90.0767 203.3584 0042307 158.5435 268.8390 13.57016165 49029
Epoch: 2026-07-27T01:25Z
TLE epoch observation values (Epoch: 2026-07-27T01:25:30.789Z)
Latitude
66.97551°
Longitude
-122.94783°
Altitude
1,058.999 km
Speed
7.328 km/s
True Right ascension
13h 32m 42s
True Declination
66° 51' 23"
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
02:16:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.994 km
Perigee altitude
1,012.196 km
Semi-major axis
7,421.732 km
Eccentricity
0.00423
Inclination
90.0767°
RAAN
203.3584°
Arg. of periapsis
158.5435°
True anomaly
268.35435°
Mean anomaly
268.839°
Eccentric anomaly
268.59667°
Mean motion
3.39457 °/min
Orbital period
106.05 mins
BSTAR
0.000073057
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|