OPS 7034 (TRANSIT 18), 3133
Orbit data source: Space-Track
OPS 7034 (TRANSIT 18), 3133 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Sat, 02 Mar 1968 UTC via an SCOUT A 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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3133 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
RCA/East Windsor
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OPS 7034 (TRANSIT 18)
1 03133U 68012A 25352.85273356 .00000104 00000-0 14195-3 0 9991
2 03133 90.0283 273.6562 0074446 151.4942 275.4365 13.51567077570013Epoch: 2025-12-18T20:27Z
TLE epoch observation values (Epoch: 2025-12-18T20:27:56.179Z)
Latitude
66.16016°
Longitude
-121.09388°
Altitude
1,073.179 km
Speed
7.324 km/s
True Right ascension
18h 14m 22s
True Declination
66° 02' 17"
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
05:13:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,118.946 km
Perigee altitude
1,008.145 km
Semi-major axis
7,441.683 km
Eccentricity
0.00744
Inclination
90.0283°
RAAN
273.6562°
Arg. of periapsis
151.4942°
True anomaly
274.58653°
Mean anomaly
275.4365°
Eccentric anomaly
275.01159°
Mean motion
3.38093 °/min
Orbital period
106.48 mins
BSTAR
0.00014195
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Other satellites on launch #12 in the year 1968 (1968-03-02 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 7034 (TRANSIT 18) 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-12-19 07:23:15.849Z | 359.803° N | 2025-12-19 07:29:15.849Z | 273.218° WNW | 44.621° | 2025-12-19 07:35:15.849Z | 188.541° SSW |
| 5 mins | 2025-12-19 17:38:15.849Z | 93.047° ESE | 2025-12-19 17:40:15.849Z | 73.559° E | 15.014° | 2025-12-19 17:43:15.849Z | 44.213° NE |
| 11 mins | 2025-12-19 19:21:15.849Z | 180.639° SSW | 2025-12-19 19:26:15.849Z | 301.99° NW | 44.65° | 2025-12-19 19:32:15.849Z | 355.929° N |
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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