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: 3 days ago
TLE from 3 days ago
0 DELTA 2 R/B(2) (PAM-D)
1 28876U 05038C 26167.79215600 .00012959 00000-0 78299-3 0 9993
2 28876 39.5515 336.7901 5067111 296.1607 20.8499 5.57876532350011Epoch: 2026-06-16T19:00Z
TLE epoch observation values (Epoch: 2026-06-16T19:00:42.278Z)
Latitude
-0.00008°
Longitude
146.54624°
Altitude
1,779.84 km
Speed
8.249 km/s
True Right ascension
22h 27m 07s
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
19:14:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
13,858.494 km
Perigee altitude
247.224 km
Semi-major axis
13,430.996 km
Eccentricity
0.50671
Inclination
39.5515°
RAAN
336.7901°
Arg. of periapsis
296.1607°
True anomaly
63.78822°
Mean anomaly
20.8499°
Eccentric anomaly
39.19874°
Mean motion
1.39438 °/min
Orbital period
258.18 mins
BSTAR
0.00078299
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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. |
|---|---|---|---|---|---|---|---|
| 74 mins | 2026-06-19 11:35:41.291Z | 164.463° S | 2026-06-19 11:49:41.291Z | 108.414° ESE | 28.725° | 2026-06-19 12:49:41.291Z | 62.198° ENE |
| 171 mins | 2026-06-19 16:02:41.291Z | 254.682° W | 2026-06-19 16:41:41.291Z | 161.067° S | 44.992° | 2026-06-19 18:53:41.291Z | 105.831° ESE |
| 166 mins | 2026-06-19 20:50:41.291Z | 292.6° NW | 2026-06-19 22:29:41.291Z | 244.668° WSW | 39.326° | 2026-06-19 23:36:41.291Z | 172.673° S |
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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