Showing default

OPS 8068, 1580

Orbit data source: Space-Track

OPS 8068, 1580 is a payload satellite owned by USAF SSD (US) in SSO that was launched on Fri, 10 Sep 1965 UTC via a THOR BURNER 1 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
1580, 1965-072A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
P35, Unknown motor
Mass
72 kg wet, 72 kg dry
Launch date (UTC)
1965-09-10 (61 years ago)
Launch vehicle
THOR BURNER 1
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 OPS 8068
1  1580U 65072A   26226.40072691  .00000131  00000-0  53757-4 0  9997
2  1580  98.4275  21.0203 0227890 233.4696 124.5312 14.29684844141330
Epoch: 2026-08-14T09:37Z
TLE epoch observation values (Epoch: 2026-08-14T09:37:02.805Z)
Latitude
0.00002°
Longitude
-86.06788°
Altitude
890.854 km
Speed
7.357 km/s
True Right ascension
01h 24m 04s
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
13:24:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
953.267 km
Perigee altitude
626.562 km
Semi-major axis
7,168.052 km
Eccentricity
0.02279
Inclination
98.4275°
RAAN
21.0203°
Arg. of periapsis
233.4696°
True anomaly
126.64785°
Mean anomaly
124.5312°
Eccentric anomaly
125.59297°
Mean motion
3.57636 °/min
Orbital period
100.66 mins
BSTAR
0.000053757
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
|