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
CYL + DISH, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 OPS 2222
1 03334U 68063A 26268.66854086 .00000040 00000-0 00000-0 0 9997
2 03334 5.6668 280.8105 0895801 235.4668 323.9308 0.99251536 27125Epoch: 2026-09-25T16:02Z
TLE epoch observation values (Epoch: 2026-09-25T16:02:41.930Z)
Latitude
-1.26656°
Longitude
-131.71596°
Altitude
33,132.358 km
Speed
3.285 km/s
True Right ascension
07h 33m 47s
True Declination
-1° 15' 55"
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
07:16:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
39,879.172 km
Perigee altitude
32,273.06 km
Semi-major axis
42,454.253 km
Eccentricity
0.08958
Inclination
5.6668°
RAAN
280.8105°
Arg. of periapsis
235.4668°
True anomaly
317.30329°
Mean anomaly
323.9308°
Eccentric anomaly
320.67844°
Mean motion
0.24812 °/min
Orbital period
1,450.91 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 | 2026-09-26 13:55:01.285Z | 227.26° WSW | 2026-09-27 04:58:01.285Z | 213.365° SW | 42.553° | 2026-09-27 13:55:01.285Z | 231.497° WSW |
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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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