Showing default

OPS 1509 (TRANSIT 10), 1864

Orbit data source: Space-Track

OPS 1509 (TRANSIT 10), 1864 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Wed, 22 Dec 1965 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
1864, 1965-109A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
51 kg wet, 51 kg dry
Launch date (UTC)
1965-12-22 (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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 OPS 1509 (TRANSIT 10)
1 01864U 65109A   26152.24712482  .00000201  00000-0  17759-3 0  9991
2 01864  89.0739 236.8939 0107434 262.6480  96.2468 13.79056904 33908
Epoch: 2026-06-01T05:55Z
TLE epoch observation values (Epoch: 2026-06-01T05:55:51.584Z)
Latitude
0.00004°
Longitude
-101.80822°
Altitude
979.653 km
Speed
7.357 km/s
True Right ascension
15h 47m 34s
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
13:10:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,043.125 km
Perigee altitude
885.361 km
Semi-major axis
7,342.38 km
Eccentricity
0.01074
Inclination
89.0739°
RAAN
236.8939°
Arg. of periapsis
262.648°
True anomaly
97.46871°
Mean anomaly
96.2468°
Eccentric anomaly
96.85795°
Mean motion
3.44975 °/min
Orbital period
104.36 mins
BSTAR
0.00017759
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
|