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.
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1580 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
P35, Unknown motor
Mass
72 kg wet, 72 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 OPS 8068
1 01580U 65072A 25305.42045268 .00000305 00000-0 10445-3 0 9995
2 01580 98.3919 104.6373 0229460 359.0391 1.0321 14.29437763100477Epoch: 2025-11-01T10:05Z
TLE epoch observation values (Epoch: 2025-11-01T10:05:27.111Z)
Latitude
-0°
Longitude
-87.67645°
Altitude
631.982 km
Speed
7.628 km/s
True Right ascension
06h 58m 32s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
04:32:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.237 km
Perigee altitude
626.242 km
Semi-major axis
7,168.876 km
Eccentricity
0.02295
Inclination
98.3919°
RAAN
104.6373°
Arg. of periapsis
359.0391°
True anomaly
1.08086°
Mean anomaly
1.0321°
Eccentric anomaly
1.05634°
Mean motion
3.57574 °/min
Orbital period
100.68 mins
BSTAR
0.00010445
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Other satellites on launch #72 in the year 1965 (1965-09-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OPS 8068 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-02 09:45:49.020Z | 108.301° ESE | 2025-11-02 09:48:49.020Z | 57.753° ENE | 21.045° | 2025-11-02 09:51:49.020Z | 16.439° NNE |
| 6 mins | 2025-11-02 11:25:49.020Z | 218.548° SW | 2025-11-02 11:27:49.020Z | 263.024° W | 28.211° | 2025-11-02 11:31:49.020Z | 326.177° NNW |
| 9 mins | 2025-11-02 23:37:49.020Z | 14.498° NNE | 2025-11-02 23:41:49.020Z | 166.551° S | 44.862° | 2025-11-02 23:46:49.020Z | 193.51° SSW |
| 4 mins | 2025-11-03 01:18:49.020Z | 317.951° NNW | 2025-11-03 01:20:49.020Z | 295.29° NW | 14.187° | 2025-11-03 01:22:49.020Z | 274.077° WNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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