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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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: 10 hours ago
TLE from 10 hours ago
0 OPS 2222
1 3334U 68063A 25354.58546170 -.00000095 00000-0 00000+0 0 9995
2 3334 6.3763 284.2129 0902200 226.9034 327.2153 0.99256778 24357Epoch: 2025-12-20T14:03Z
TLE epoch observation values (Epoch: 2025-12-20T14:03:03.890Z)
Latitude
-0.86428°
Longitude
171.97225°
Altitude
32,968.858 km
Speed
3.297 km/s
True Right ascension
07h 28m 35s
True Declination
0° 51' 48"
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
23:16:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
39,904.705 km
Perigee altitude
32,244.53 km
Semi-major axis
42,452.754 km
Eccentricity
0.09022
Inclination
6.3763°
RAAN
284.2129°
Arg. of periapsis
226.9034°
True anomaly
321.04569°
Mean anomaly
327.2153°
Eccentric anomaly
324.19085°
Mean motion
0.24813 °/min
Orbital period
1,450.84 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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