Showing default

OPS 5712 (P/L 160), 2826

Orbit data source: Space-Track

OPS 5712 (P/L 160), 2826 is a payload satellite owned by NRL (US) in LEO that was launched on Wed, 31 May 1967 UTC via a THOR SLV-2 AGENA D 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
2826, 1967-053A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Operational Defense Calibration
Bus & Motor
NRL 14"?, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
1967-05-31 (58 years ago)
Launch vehicle
THOR SLV-2 AGENA D
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere, 0.3 m
Radar Cross Section
0.204 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 OPS 5712 (P/L 160)
1 02826U 67053A   25242.11878772  .00013653  00000-0  21999-2 0  9995
2 02826  69.9207  28.6095 0001008  70.9754 289.1500 14.71588659 23312
Epoch: 2025-08-30T02:51Z
TLE epoch observation values (Epoch: 2025-08-30T02:51:03.258Z)
Latitude
-0.00003°
Longitude
7.28825°
Altitude
658.158 km
Speed
7.529 km/s
True Right ascension
01h 54m 26s
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
15:50:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.691 km
Perigee altitude
653.273 km
Semi-major axis
7,032.119 km
Eccentricity
0.0001
Inclination
69.9207°
RAAN
28.6095°
Arg. of periapsis
70.9754°
True anomaly
289.13909°
Mean anomaly
289.15°
Eccentric anomaly
289.14454°
Mean motion
3.68056 °/min
Orbital period
97.81 mins
BSTAR
0.0021999
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
|