SBS 3 R/B(PAM-D), 13658
Orbit data source: Space-Track
SBS 3 R/B(PAM-D), 13658 is space debris in HEO originally from a launch on Thu, 11 Nov 1982 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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13658 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
2 days ago
Origin
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 48, Unknown motor
Mass
2,154 kg wet, 191 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Sphere + Cone, 1.8 m
Radar Cross Section
2.046 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 2 days ago
0 SBS 3 R/B(PAM-D)
1 13658U 82110D 25195.33486938 .00000853 00000-0 63139-3 0 9992
2 13658 23.3739 97.5747 7081344 155.5946 268.4843 2.49499246293876Epoch: 2025-07-14T08:02Z
TLE epoch observation values (Epoch: 2025-07-14T08:02:12.714Z)
Latitude
0.00007°
Longitude
44.53849°
Altitude
25,891.29 km
Speed
2.71 km/s
True Right ascension
06h 30m 08s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-5.22349°
Longitude
31.54902°
Altitude
31,532.748 km
Speed
1.916 km/s
Apparent Right ascension
05h 50m 15s
Apparent Declination
-10° 06' 25"
Sunlit
Visualization observer readout
Local Sidereal Time
19:25:59
Azimuth
42.051° NE
Elevation
-53.394°
Doppler factor
1
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Other satellites on launch #110 in the year 1982 (1982-11-11 UTC)
SBS 3 R/B(PAM-D) Visibility forecast
Observer location: undefined°, undefined°
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. |
|---|---|---|---|---|---|---|---|
| 467 mins | 2025-07-16 12:03:00.414Z | 154.772° SSE | 2025-07-16 19:10:00.414Z | 163.035° S | 36.922° | 2025-07-16 19:50:00.414Z | 102.017° ESE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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