OPS 0340, 2125
Orbit data source: Space-Track
OPS 0340, 2125 is a payload satellite owned by USAF SSD (US) in SSO that was launched on Thu, 31 Mar 1966 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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2125 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 0340
1 02125U 66026A 25315.02587988 .00001867 00000-0 34134-3 0 9993
2 02125 98.0130 125.0543 0146724 208.7348 150.5714 14.60345481127705Epoch: 2025-11-11T00:37Z
TLE epoch observation values (Epoch: 2025-11-11T00:37:16.021Z)
Latitude
0.00003°
Longitude
65.31919°
Altitude
785.781 km
Speed
7.413 km/s
True Right ascension
08h 20m 13s
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
22:41:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
792.824 km
Perigee altitude
585.436 km
Semi-major axis
7,067.267 km
Eccentricity
0.01467
Inclination
98.013°
RAAN
125.0543°
Arg. of periapsis
208.7348°
True anomaly
151.38448°
Mean anomaly
150.5714°
Eccentric anomaly
150.97923°
Mean motion
3.65314 °/min
Orbital period
98.55 mins
BSTAR
0.00034134
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Other satellites on launch #26 in the year 1966 (1966-03-31 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 0340 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-12 11:15:41.291Z | 157.709° S | 2025-11-12 11:20:41.291Z | 83.817° E | 43.456° | 2025-11-12 11:25:41.291Z | 352.196° N |
| 4 mins | 2025-11-12 23:17:41.291Z | 67.916° E | 2025-11-12 23:18:41.291Z | 83.39° E | 15.979° | 2025-11-12 23:21:41.291Z | 129.151° SE |
| 6 mins | 2025-11-13 00:54:41.291Z | 344.125° N | 2025-11-13 00:56:41.291Z | 299.14° NW | 32.795° | 2025-11-13 01:00:41.291Z | 221.143° SW |
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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