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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Iframe URL

https://www.satcat.com/sats-embedded/35492?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

35492, 2009-033B

Orbit

HEO

Last TLE update

15 hours ago

Origin

United Launch Alliance/Lockheed Martin (US)

Manufacturer

ULA Decatur

Mission

2))"

Bus & Motor

DCSS-4, RL10B-2

Mass

2,850 kg wet, 2,850 kg dry

Launch date (UTC)

2009-06-27 (16 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, Unknown HBR

Radar Cross Section

43.982 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 15 hours ago

0 DELTA 4 R/B
1 35492U 09033B   25128.63964737 -.00000041  00000-0  00000-0 0  9997
2 35492  12.7359 129.8708 5167182  38.3155  94.3327  1.93162106111945

Epoch: 2025-05-08T15:21Z

Definitive object data (Epoch: 2025-05-08T15:21:05.532Z)

Latitude

-0.48624°

Longitude

-144.96547°

Altitude

27,849.822 km

Speed

2.942 km/s

True Right ascension

20h 48m 03s

True Declination

0° 29' 08"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-7.25199°

Longitude

-112.90069°

Altitude

34,829.366 km

Speed

2.17 km/s

Apparent Right ascension

23h 17m 04s

Apparent Declination

-11° 54' 49"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:33:02

Azimuth

71.042° E

Elevation

-38.674°

Doppler factor

Orbital elements

Apogee altitude

34,932.683 km

Perigee altitude

6,784.999 km

Semi-major axis

27,236.978 km

Eccentricity

0.5167182

Inclination

12.7359°

RAAN

129.8708°

Arg. of periapsis

38.3155°

True anomaly

143.88309°

Mean anomaly

94.3327°

Eccentric anomaly

119.97779°

Mean motion

0.48284 °/min

BSTAR

Unknown

Orbital period

745.59 mins

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Other satellites on launch #33 in the year 2009 (2009-06-27 UTC)

GOES 14, 35491

DELTA 4 R/B 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.
216 mins	2025-05-09 14:41:12.573Z	256.478° W	2025-05-09 16:00:12.573Z	244.882° WSW	15.904°	2025-05-09 18:17:12.573Z	244.079° WSW
71 mins	2025-05-10 00:29:12.573Z	224.526° SW	2025-05-10 01:12:12.573Z	165.087° S	25.949°	2025-05-10 01:40:12.573Z	108.075° ESE

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Check out DELTA 4 R/B, 35492 on other resources

View DELTA 4 R/B, 35492 on Heavens-Above

View DELTA 4 R/B, 35492 on Keep Track

View DELTA 4 R/B, 35492 on Celestrak

View DELTA 4 R/B, 35492 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.