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: 19 hours ago
TLE from 19 hours ago
0 OPS 0340
1 02125U 66026A 25353.05196369 .00000501 00000-0 97677-4 0 9993
2 02125 98.0130 161.8561 0148336 89.8564 271.9634 14.60463409133259Epoch: 2025-12-19T01:14Z
TLE epoch observation values (Epoch: 2025-12-19T01:14:49.662Z)
Latitude
-0.00003°
Longitude
55.25052°
Altitude
692.632 km
Speed
7.511 km/s
True Right ascension
10h 47m 25s
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
18:59:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
793.577 km
Perigee altitude
583.922 km
Semi-major axis
7,066.886 km
Eccentricity
0.01483
Inclination
98.013°
RAAN
161.8561°
Arg. of periapsis
89.8564°
True anomaly
270.26376°
Mean anomaly
271.9634°
Eccentric anomaly
271.11366°
Mean motion
3.65343 °/min
Orbital period
98.54 mins
BSTAR
0.000097677
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-19 23:13:03.274Z | 59.543° ENE | 2025-12-19 23:15:03.274Z | 89.173° E | 15.34° | 2025-12-19 23:17:03.274Z | 120.386° SE |
| 6 mins | 2025-12-20 00:51:03.274Z | 340.984° N | 2025-12-20 00:53:03.274Z | 286.461° WNW | 33.305° | 2025-12-20 00:57:03.274Z | 218.402° SW |
| 6 mins | 2025-12-20 11:55:03.274Z | 203.392° SW | 2025-12-20 11:57:03.274Z | 252.985° W | 33.74° | 2025-12-20 12:01:03.274Z | 331.692° 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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