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: 20 hours ago
TLE from 20 hours ago
0 OPS 0340
1 02125U 66026A 26073.48199098 .00001373 00000-0 25169-3 0 9996
2 02125 98.0233 244.6000 0146691 181.3117 178.7720 14.60639388145721Epoch: 2026-03-14T11:34Z
TLE epoch observation values (Epoch: 2026-03-14T11:34:04.020Z)
Latitude
-0.00006°
Longitude
-101.01928°
Altitude
797.8 km
Speed
7.4 km/s
True Right ascension
16h 18m 24s
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
11:54:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
791.838 km
Perigee altitude
584.525 km
Semi-major axis
7,066.319 km
Eccentricity
0.01467
Inclination
98.0233°
RAAN
244.6°
Arg. of periapsis
181.3117°
True anomaly
178.80738°
Mean anomaly
178.772°
Eccentric anomaly
178.78975°
Mean motion
3.65387 °/min
Orbital period
98.53 mins
BSTAR
0.00025169
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-03-15 10:42:14.761Z | 139.142° SSE | 2026-03-15 10:47:14.761Z | 63.606° ENE | 32.736° | 2026-03-15 10:51:14.761Z | 4.632° NNE |
| 6 mins | 2026-03-15 12:22:14.761Z | 229.506° WSW | 2026-03-15 12:24:14.761Z | 259.659° W | 21.416° | 2026-03-15 12:28:14.761Z | 315.543° NNW |
| 6 mins | 2026-03-16 00:20:14.761Z | 7.666° NNE | 2026-03-16 00:22:14.761Z | 344.474° N | 42.793° | 2026-03-16 00:26:14.761Z | 198.914° SSW |
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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