OPS 9326 (IDSCS 13), 2653
Orbit data source: Space-Track
OPS 9326 (IDSCS 13), 2653 is a payload satellite owned by USAF SSD (US) in GEO that was launched on Wed, 18 Jan 1967 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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2653 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Philco-Ford WDL
Mission
Non-operational spacecraft
Bus & Motor
IDCSP, Unknown motor
Mass
45 kg wet, 45 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
ICO POLY, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 OPS 9326 (IDSCS 13)
1 02653U 67003F 26263.69746785 -.00000057 00000-0 00000-0 0 9996
2 02653 8.3633 45.2978 0044924 68.3635 292.2062 1.07748643133729Epoch: 2026-09-20T16:44Z
TLE epoch observation values (Epoch: 2026-09-20T16:44:21.222Z)
Latitude
0°
Longitude
154.69367°
Altitude
33,745.488 km
Speed
3.155 km/s
True Right ascension
03h 01m 28s
True Declination
0° 00' 00"
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
09:14:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,994.367 km
Perigee altitude
33,633.251 km
Semi-major axis
40,191.946 km
Eccentricity
0.00449
Inclination
8.3633°
RAAN
45.2978°
Arg. of periapsis
68.3635°
True anomaly
291.72858°
Mean anomaly
292.2062°
Eccentric anomaly
291.96749°
Mean motion
0.26936 °/min
Orbital period
1,336.5 mins
BSTAR
0
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Other satellites on launch #3 in the year 1967 (1967-01-18 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 9326 (IDSCS 13) 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. |
|---|---|---|---|---|---|---|---|
| 613 mins | 2026-09-21 18:35:59.179Z | 263.245° W | 2026-09-21 22:52:59.179Z | 258.731° W | 14.316° | 2026-09-22 04:48:59.179Z | 244.825° WSW |
| 533 mins | 2026-09-22 07:19:59.179Z | 240.915° WSW | 2026-09-22 16:12:59.179Z | 244.111° WSW | 28.051° | 2026-09-22 16:12:59.179Z | 244.111° WSW |
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2653 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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