DELTA 2 R/B(2) (PAM-D), 28876
Orbit data source: Space-Track
DELTA 2 R/B(2) (PAM-D), 28876 is space debris in HEO originally from a launch on Mon, 26 Sep 2005 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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28876 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ATK/Elkton
Mission
Spacecraft
Bus & Motor
STAR 48, Unknown motor
Mass
133 kg wet, 132 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Sphere + Cone, 1.1 m
Radar Cross Section
2.822 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 DELTA 2 R/B(2) (PAM-D)
1 28876U 05038C 26166.00007466 .00013142 00000-0 80529-3 0 9999
2 28876 39.5525 338.6313 5067008 293.8093 21.8681 5.57831507349912Epoch: 2026-06-15T00:00Z
TLE epoch observation values (Epoch: 2026-06-15T00:00:06.450Z)
Latitude
0.00009°
Longitude
75.30509°
Altitude
1,908.827 km
Speed
8.157 km/s
True Right ascension
22h 34m 29s
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
03:42:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
13,859.444 km
Perigee altitude
247.719 km
Semi-major axis
13,431.719 km
Eccentricity
0.5067
Inclination
39.5525°
RAAN
338.6313°
Arg. of periapsis
293.8093°
True anomaly
66.13015°
Mean anomaly
21.8681°
Eccentric anomaly
40.86177°
Mean motion
1.39427 °/min
Orbital period
258.2 mins
BSTAR
0.00080529
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Other satellites on launch #38 in the year 2005 (2005-09-26 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.DELTA 2 R/B(2) (PAM-D) 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. |
|---|---|---|---|---|---|---|---|
| 179 mins | 2026-06-15 17:29:25.665Z | 265.311° W | 2026-06-15 18:34:25.665Z | 175.414° S | 44.994° | 2026-06-15 20:28:25.665Z | 118.312° SE |
| 150 mins | 2026-06-15 22:29:25.665Z | 296.611° NW | 2026-06-16 00:05:25.665Z | 256.306° W | 32.915° | 2026-06-16 00:59:25.665Z | 193.882° SSW |
| 21 mins | 2026-06-16 10:37:25.665Z | 104.689° ESE | 2026-06-16 10:44:25.665Z | 90.088° ESE | 12.222° | 2026-06-16 10:58:25.665Z | 72.858° E |
| 136 mins | 2026-06-16 14:51:25.665Z | 230.885° WSW | 2026-06-16 15:16:25.665Z | 151.229° SSE | 44.43° | 2026-06-16 17:07:25.665Z | 84.189° E |
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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