DELTA 4 R/B, 35492
Orbit data source: Space-Track
DELTA 4 R/B, 35492 is space debris in HEO originally from a launch on Sat, 27 Jun 2009 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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35492 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ULA Decatur
Mission
Spacecraft
Bus & Motor
DCSS-4, RL10B-2
Mass
2,850 kg wet, 2,850 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 6.0 m
Radar Cross Section
43.982 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 DELTA 4 R/B
1 35492U 09033B 26083.89979071 -.00000167 00000-0 00000-0 0 9992
2 35492 13.0156 90.9937 5213756 111.5206 315.5923 1.93161132118132Epoch: 2026-03-24T21:35Z
TLE epoch observation values (Epoch: 2026-03-24T21:35:41.917Z)
Latitude
1.28256°
Longitude
-49.65232°
Altitude
16,681.29 km
Speed
4.465 km/s
True Right ascension
06h 26m 34s
True Declination
1° 16' 49"
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
20:32:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,059.699 km
Perigee altitude
6,658.196 km
Semi-major axis
27,237.085 km
Eccentricity
0.52138
Inclination
13.0156°
RAAN
90.9937°
Arg. of periapsis
111.5206°
True anomaly
254.35407°
Mean anomaly
315.5923°
Eccentric anomaly
287.02947°
Mean motion
0.48284 °/min
Orbital period
745.59 mins
BSTAR
0
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Other satellites on launch #33 in the year 2009 (2009-06-27 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 4 R/B 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. |
|---|---|---|---|---|---|---|---|
| 457 mins | 2026-03-25 15:20:29.963Z | 130.57° SE | 2026-03-25 21:12:29.963Z | 140.693° SSE | 23.883° | 2026-03-25 22:57:29.963Z | 109.032° ESE |
| 166 mins | 2026-03-26 12:34:29.963Z | 245.978° WSW | 2026-03-26 13:09:29.963Z | 187.408° SSW | 26.905° | 2026-03-26 15:20:29.963Z | 143.028° SSE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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