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

1 day 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 1 day ago

0 DELTA 4 R/B
1 35492U 09033B   25183.47104435 -.00000055  00000-0  00000-0 0  9996
2 35492  12.7673 123.4334 5171536  50.6299  62.6940  1.93162028113004

Epoch: 2025-07-02T11:18Z

TLE epoch observation values (Epoch: 2025-07-02T11:18:18.231Z)

Latitude

1.37552°

Longitude

-153.0659°

Altitude

21,436.563 km

Speed

3.745 km/s

True Right ascension

19h 49m 02s

True Declination

1° 22' 24"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-2.28985°

Longitude

-136.96077°

Altitude

26,503.945 km

Speed

3.1 km/s

Apparent Right ascension

20h 22m 12s

Apparent Declination

-9° 59' 46"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:45:17

Azimuth

246.394° WSW

Elevation

11.455°

Doppler factor

Orbital elements

Apogee altitude

34,944.555 km

Perigee altitude

6,773.144 km

Semi-major axis

27,236.986 km

Eccentricity

0.51715

Inclination

12.7673°

RAAN

123.4334°

Arg. of periapsis

50.6299°

True anomaly

Unknown

Mean anomaly

62.694°

Eccentric anomaly

Unknown

Mean motion

0.48284 °/min

Orbital period

745.59 mins

BSTAR

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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.
60 mins	2025-07-03 12:58:32.482Z	246.376° WSW	2025-07-03 13:03:32.482Z	246.057° WSW	11.235°	2025-07-03 13:58:32.482Z	244.404° WSW
74 mins	2025-07-03 21:32:32.482Z	229.319° WSW	2025-07-03 22:15:32.482Z	168.343° S	28.802°	2025-07-03 22:46:32.482Z	105.551° 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.