OPS 9345 (IDSCS 23), 3288
Orbit data source: Space-Track
OPS 9345 (IDSCS 23), 3288 is a payload satellite owned by SAMSO (US) in GEO that was launched on Thu, 13 Jun 1968 UTC via a TITAN IIIC 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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3288 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Philco-Ford
Mission
Non-operational Defense Communications
Bus & Motor
IDCSP, Unknown motor
Mass
45 kg wet, 45 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Poly, 0.5 m
Radar Cross Section
0.926 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OPS 9345 (IDSCS 23)
1 03288U 68050E 25255.13147348 -.00000104 00000-0 00000-0 0 9996
2 03288 6.5250 55.3253 0036207 135.4642 69.0745 1.07478759136253Epoch: 2025-09-12T03:09Z
TLE epoch observation values (Epoch: 2025-09-12T03:09:19.308Z)
Latitude
-2.72954°
Longitude
-138.61496°
Altitude
33,828.35 km
Speed
3.151 km/s
True Right ascension
17h 20m 23s
True Declination
-2° 43' 36"
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
19:12:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,026.84 km
Perigee altitude
33,735.307 km
Semi-major axis
40,259.21 km
Eccentricity
0.00362
Inclination
6.525°
RAAN
55.3253°
Arg. of periapsis
135.4642°
True anomaly
69.46266°
Mean anomaly
69.0745°
Eccentric anomaly
69.26852°
Mean motion
0.26869 °/min
Orbital period
1,339.85 mins
BSTAR
0
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Other satellites on launch #50 in the year 1968 (1968-06-13 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 9345 (IDSCS 23) 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 | 2025-09-13 02:43:08.042Z | 191.349° SSW | 2025-09-13 16:25:08.042Z | 168.913° S | 37.58° | 2025-09-14 02:43:08.042Z | 156.041° SSE |
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3288 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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