DELTA 4 R/B, 29156

Orbit data source: Space-Track

DELTA 4 R/B, 29156 is space debris in HEO originally from a launch on Wed, 24 May 2006 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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https://www.satcat.com/sats-embedded/29156?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29156, 2006-018B

Orbit

HEO

Last TLE update

1 day ago

Origin

Boeing (US)

Manufacturer

ULA Decatur

Mission

2))"

Bus & Motor

DCSS-4, RL10B-2

Mass

2,850 kg wet, 2,850 kg dry

Launch date (UTC)

2006-05-24 (19 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 29156U 06018B   25115.24959981 -.00000037  00000-0  00000-0 0  9990
2 29156  13.3751 315.4884 5247006 301.0361  15.4717  1.93074984133395

Epoch: 2025-04-25T05:59Z

Definitive object data (Epoch: 2025-04-25T05:59:25.423Z)

Latitude

-1.33872°

Longitude

6.43193°

Altitude

8,653.812 km

Speed

6.197 km/s

True Right ascension

20h 39m 11s

True Declination

-1° 20' 06"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

11.37506°

Longitude

134.21136°

Altitude

35,153.818 km

Speed

2.136 km/s

Apparent Right ascension

05h 26m 39s

Apparent Declination

5° 16' 22"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

19:52:03

Azimuth

45.246° ENE

Elevation

-33.792°

Doppler factor

Orbital elements

Apogee altitude

35,162.622 km

Perigee altitude

6,571.486 km

Semi-major axis

27,245.191 km

Eccentricity

0.5247006

Inclination

13.3751°

RAAN

315.4884°

Arg. of periapsis

301.0361°

True anomaly

52.70187°

Mean anomaly

15.4717°

Eccentric anomaly

30.91884°

Mean motion

0.48262 °/min

BSTAR

Unknown

Orbital period

745.92 mins

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Other satellites on launch #18 in the year 2006 (2006-05-24 UTC)

GOES 13, 29155

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.
649 mins	2025-04-26 19:57:27.974Z	255.628° W	2025-04-26 22:30:27.974Z	243.513° WSW	32.09°	2025-04-27 06:46:27.974Z	175.595° S

Authenticating...

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Check out DELTA 4 R/B, 29156 on other resources

View DELTA 4 R/B, 29156 on Heavens-Above

View DELTA 4 R/B, 29156 on Keep Track

View DELTA 4 R/B, 29156 on Celestrak

View DELTA 4 R/B, 29156 on Gunter's Space Page

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