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

19 hours 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 19 hours ago

0 DELTA 4 R/B
1 29156U 06018B   25121.87859510 -.00000231  00000-0  00000+0 0  9998
2 29156  13.3644 314.7715 5247785 302.4687 303.0781  1.93076417133582

Epoch: 2025-05-01T21:05Z

Definitive object data (Epoch: 2025-05-01T21:05:10.616Z)

Latitude

-0.81915°

Longitude

-38.1945°

Altitude

20,058.912 km

Speed

3.94 km/s

True Right ascension

09h 12m 34s

True Declination

0° 49' 04"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

12.63611°

Longitude

-112.16764°

Altitude

33,929.145 km

Speed

2.269 km/s

Apparent Right ascension

04h 43m 18s

Apparent Declination

7° 14' 38"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:09:14

Azimuth

98.406° ESE

Elevation

21.073°

Doppler factor

Orbital elements

Apogee altitude

35,164.54 km

Perigee altitude

6,569.3 km

Semi-major axis

27,245.057 km

Eccentricity

0.5247785

Inclination

13.3644°

RAAN

314.7715°

Arg. of periapsis

302.4687°

True anomaly

240.98268°

Mean anomaly

303.0781°

Eccentric anomaly

273.05319°

Mean motion

0.48263 °/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.
340 mins	2025-05-02 16:26:21.267Z	98.423° ESE	2025-05-02 19:31:21.267Z	112.008° ESE	24.565°	2025-05-02 22:06:21.267Z	115.655° SE
231 mins	2025-05-03 12:35:21.267Z	206.957° SW	2025-05-03 13:20:21.267Z	141.684° SSE	28.77°	2025-05-03 16:26:21.267Z	106.456° ESE

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.