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 spacecraft
Bus & Motor
NRL 14"?, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
1967-05-31 (59 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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 OPS 5712 (P/L 160)
1 02826U 67053A   26072.96706918  .00009288  00000-0  13478-2 0  9994
2 02826  69.9162 271.4309 0003933 220.3160 139.7696 14.76262611 52173
Epoch: 2026-03-13T23:12Z
TLE epoch observation values (Epoch: 2026-03-13T23:12:34.777Z)
Latitude
Longitude
111.69099°
Altitude
645.649 km
Speed
7.534 km/s
True Right ascension
18h 05m 43s
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
09:55:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.883 km
Perigee altitude
636.364 km
Semi-major axis
7,017.261 km
Eccentricity
0.00039
Inclination
69.9162°
RAAN
271.4309°
Arg. of periapsis
220.316°
True anomaly
139.7987°
Mean anomaly
139.7696°
Eccentric anomaly
139.78415°
Mean motion
3.69226 °/min
Orbital period
97.5 mins
BSTAR
0.0013478
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
|