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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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: 18 hours ago
TLE from 18 hours ago
0 OPS 2222
1 03334U 68063A 26112.02032709 -.00000148 00000-0 00000-0 0 9995
2 03334 6.0612 282.7332 0895247 230.3729 153.5934 0.99249866 25570Epoch: 2026-04-22T00:29Z
TLE epoch observation values (Epoch: 2026-04-22T00:29:16.260Z)
Latitude
2.87548°
Longitude
93.32135°
Altitude
39,525.989 km
Speed
2.825 km/s
True Right ascension
20h 42m 54s
True Declination
2° 52' 22"
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
01:17:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
39,877.336 km
Perigee altitude
32,275.843 km
Semi-major axis
42,454.727 km
Eccentricity
0.08952
Inclination
6.0612°
RAAN
282.7332°
Arg. of periapsis
230.3729°
True anomaly
157.73537°
Mean anomaly
153.5934°
Eccentric anomaly
155.7039°
Mean motion
0.24812 °/min
Orbital period
1,450.94 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
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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. |
|---|---|---|---|---|---|---|---|
| OPS 2222 is likely not visible in the next few days. |
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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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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