Showing default

OPS 8464 (TRANSIT 5B-7), 1514

Orbit data source: Space-Track

OPS 8464 (TRANSIT 5B-7), 1514 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Fri, 13 Aug 1965 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
1514, 1965-065F
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NAFI
Mission
Defense Navigation
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~54 kg wet, ~54 kg dry
Launch date (UTC)
1965-08-13 (60 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 + 1 Rod, Unknown HBR
Radar Cross Section
7.565 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 OPS 8464 (TRANSIT 5B-7)
1 01514U 65065F   25259.96538215  .00000095  00000-0  16739-3 0  9998
2 01514  89.9761 228.1996 0068918 209.0432 212.7193 13.35313829924808
Epoch: 2025-09-16T23:10Z
TLE epoch observation values (Epoch: 2025-09-16T23:10:09.017Z)
Latitude
61.42527°
Longitude
-115.44243°
Altitude
1,180.996 km
Speed
7.248 km/s
True Right ascension
15h 12m 58s
True Declination
61° 17' 19"
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
16:58:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,175.56 km
Perigee altitude
1,072.155 km
Semi-major axis
7,501.995 km
Eccentricity
0.00689
Inclination
89.9761°
RAAN
228.1996°
Arg. of periapsis
209.0432°
True anomaly
212.2955°
Mean anomaly
212.7193°
Eccentric anomaly
212.50709°
Mean motion
3.34024 °/min
Orbital period
107.78 mins
BSTAR
0.00016739
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
|