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: 1 day ago
TLE from 1 day ago
0 OPS 8068
1 1580U 65072A 25306.47039199 .00000256 00000-0 90034-4 0 9995
2 1580 98.3919 105.6500 0229385 355.9349 3.9964 14.29438228100622Epoch: 2025-11-02T11:17Z
TLE epoch observation values (Epoch: 2025-11-02T11:17:21.867Z)
Latitude
-0.0001°
Longitude
-105.67675°
Altitude
632.425 km
Speed
7.628 km/s
True Right ascension
07h 02m 36s
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
07:35:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
955.181 km
Perigee altitude
626.295 km
Semi-major axis
7,168.875 km
Eccentricity
0.02294
Inclination
98.3919°
RAAN
105.65°
Arg. of periapsis
355.9349°
True anomaly
4.18498°
Mean anomaly
3.9964°
Eccentric anomaly
4.09014°
Mean motion
3.57575 °/min
Orbital period
100.68 mins
BSTAR
0.000090034
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-03 23:07:42.356Z | 24.625° NE | 2025-11-03 23:12:42.356Z | 84.562° E | 37.392° | 2025-11-03 23:18:42.356Z | 174.141° S |
| 7 mins | 2025-11-04 00:49:42.356Z | 331.266° NNW | 2025-11-04 00:52:42.356Z | 288.989° WNW | 22.816° | 2025-11-04 00:56:42.356Z | 244.567° WSW |
| 7 mins | 2025-11-04 10:27:42.356Z | 148.188° SSE | 2025-11-04 10:30:42.356Z | 71.113° E | 41.283° | 2025-11-04 10:34:42.356Z | 355.371° N |
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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