OPS 9432 (DSCS 2-2), 5588
Orbit data source: Space-Track
OPS 9432 (DSCS 2-2), 5588 is an American payload satellite in GEO that was launched on Wed, 03 Nov 1971 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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5588 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
TRW
Mission
Non-operational spacecraft
Bus & Motor
DSCS II, Unknown motor
Mass
526 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OPS 9432 (DSCS 2-2)
1 5588U 71095B 26271.92197624 -.00000258 00000-0 00000+0 0 9991
2 5588 1.2956 251.1205 0003006 44.6346 140.8109 1.00155605 48405Epoch: 2026-09-28T22:07Z
TLE epoch observation values (Epoch: 2026-09-28T22:07:38.747Z)
Latitude
-0.14623°
Longitude
96.95209°
Altitude
35,828.468 km
Speed
3.073 km/s
True Right ascension
05h 06m 13s
True Declination
0° 08' 46"
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
05:22:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,832.95 km
Perigee altitude
35,807.58 km
Semi-major axis
42,198.402 km
Eccentricity
0.0003
Inclination
1.2956°
RAAN
251.1205°
Arg. of periapsis
44.6346°
True anomaly
140.83266°
Mean anomaly
140.8109°
Eccentric anomaly
140.82178°
Mean motion
0.25038 °/min
Orbital period
1,437.82 mins
BSTAR
0
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Other satellites on launch #95 in the year 1971 (1971-11-03 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 9432 (DSCS 2-2) 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. |
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| OPS 9432 (DSCS 2-2) is likely not visible in the next few days. |
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5588 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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