Showing default

OPS 1593 (TRANSIT 11), 1952

Orbit data source: Space-Track

OPS 1593 (TRANSIT 11), 1952 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Fri, 28 Jan 1966 UTC via an SCOUT A 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
1952, 1966-005A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NAFI
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
1966-01-28 (60 years ago)
Launch vehicle
SCOUT A
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: 18 hours ago

TLE from 18 hours ago
0 OPS 1593 (TRANSIT 11)
1 01952U 66005A   26080.21865579  .00000164  00000-0  15752-3 0  9997
2 01952  90.1541 350.4658 0215196 281.7183  75.9906 13.68110549994123
Epoch: 2026-03-21T05:14Z
TLE epoch observation values (Epoch: 2026-03-21T05:14:51.860Z)
Latitude
0.00002°
Longitude
93.0072°
Altitude
974.111 km
Speed
7.382 km/s
True Right ascension
23h 21m 51s
True Declination
0° 00' 00"
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
03:52:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,162.231 km
Perigee altitude
844.536 km
Semi-major axis
7,381.521 km
Eccentricity
0.02152
Inclination
90.1541°
RAAN
350.4658°
Arg. of periapsis
281.7183°
True anomaly
78.39819°
Mean anomaly
75.9906°
Eccentric anomaly
77.19291°
Mean motion
3.42235 °/min
Orbital period
105.19 mins
BSTAR
0.00015752
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
|