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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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: 10 hours ago
TLE from 10 hours ago
0 OPS 0340
1 02125U 66026A 26048.40856116 .00000916 00000-0 17225-3 0 9997
2 02125 98.0192 220.3009 0145539 260.3904 98.0828 14.60570972142067Epoch: 2026-02-17T09:48Z
TLE epoch observation values (Epoch: 2026-02-17T09:48:19.684Z)
Latitude
-0.00003°
Longitude
-74.17009°
Altitude
710.256 km
Speed
7.492 km/s
True Right ascension
14h 41m 12s
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
23:09:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.248 km
Perigee altitude
585.557 km
Semi-major axis
7,066.539 km
Eccentricity
0.01455
Inclination
98.0192°
RAAN
220.3009°
Arg. of periapsis
260.3904°
True anomaly
99.72955°
Mean anomaly
98.0828°
Eccentric anomaly
98.90662°
Mean motion
3.6537 °/min
Orbital period
98.53 mins
BSTAR
0.00017225
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-17 23:33:18.791Z | 36.713° NE | 2026-02-17 23:37:18.791Z | 104.832° ESE | 28.973° | 2026-02-17 23:40:18.791Z | 154.086° SSE |
| 6 mins | 2026-02-18 01:11:18.791Z | 339.792° N | 2026-02-18 01:14:18.791Z | 293.28° NW | 24.076° | 2026-02-18 01:17:18.791Z | 245.735° WSW |
| 7 mins | 2026-02-18 10:37:18.791Z | 118.602° SE | 2026-02-18 10:40:18.791Z | 61.696° ENE | 28.997° | 2026-02-18 10:44:18.791Z | 7.579° NNE |
| 7 mins | 2026-02-18 12:14:18.791Z | 215.071° SW | 2026-02-18 12:17:18.791Z | 261.197° W | 25.176° | 2026-02-18 12:21:18.791Z | 319.872° NNW |
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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