OPS 2222, 3334
Orbit data source: Space-Track
OPS 2222, 3334 is an American payload satellite in GEO that was launched on Tue, 06 Aug 1968 UTC via an ATLAS SLV-3A AGENA D launch vehicle from the Air Force Eastern Test Range (AFETR). 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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3334 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
LMSC?
Mission
Non-operational spacecraft
Bus & Motor
CANYON, Unknown motor
Mass
~240 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 OPS 2222
1 03334U 68063A 25323.79202986 -.00000232 00000-0 00000-0 0 9992
2 03334 6.4572 284.5937 0906103 225.9931 124.8048 0.99252719 24048Epoch: 2025-11-19T19:00Z
TLE epoch observation values (Epoch: 2025-11-19T19:00:31.379Z)
Latitude
-0.14154°
Longitude
-60.88393°
Altitude
38,466.625 km
Speed
2.896 km/s
True Right ascension
18h 53m 13s
True Declination
0° 08' 29"
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
12:41:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
39,922.536 km
Perigee altitude
32,229.013 km
Semi-major axis
42,453.911 km
Eccentricity
0.09061
Inclination
6.4572°
RAAN
284.5937°
Arg. of periapsis
225.9931°
True anomaly
132.78594°
Mean anomaly
124.8048°
Eccentric anomaly
128.84807°
Mean motion
0.24812 °/min
Orbital period
1,450.89 mins
BSTAR
0
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Other satellites on launch #63 in the year 1968 (1968-08-06 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 2222 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-11-20 15:42:31.144Z | 127.787° SE | 2025-11-21 03:41:31.144Z | 143.822° SSE | 35.274° | 2025-11-21 15:42:31.144Z | 131.455° SE |
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3334 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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