DELTA 1 DEB, 29010

Orbit data source: Space-Track

DELTA 1 DEB, 29010 is space debris in LEO originally from a launch on Sat, 06 Nov 1965 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/29010?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29010, 1965-089H

Orbit

LEO

Last TLE update

4 weeks ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1965-11-06 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 4 weeks ago

0 DELTA 1 DEB
1 29010U 65089H   25103.47924407 -.00001662  00000-0 -89937-2 0  9993
2 29010  59.2705 359.8486 0663758 249.9756 292.0496 12.09188555473024

Epoch: 2025-04-13T11:30Z

Definitive object data (Epoch: 2025-04-13T11:30:06.687Z)

Latitude

4.43968°

Longitude

162.78039°

Altitude

1,472.477 km

Speed

7.202 km/s

True Right ascension

11h 48m 51s

True Declination

4° 24' 56"

Sunlit

Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude

2.77515°

Longitude

104.29862°

Altitude

1,614.991 km

Speed

7.075 km/s

Apparent Right ascension

06h 05m 14s

Apparent Declination

-19° 38' 58"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:50:38

Azimuth

281.306° WNW

Elevation

-43.868°

Doppler factor

Orbital elements

Apogee altitude

2,171.557 km

Perigee altitude

1,107.218 km

Semi-major axis

8,017.525 km

Eccentricity

0.0663758

Inclination

59.2705°

RAAN

359.8486°

Arg. of periapsis

249.9756°

True anomaly

284.79299°

Mean anomaly

292.0496°

Eccentric anomaly

288.44185°

Mean motion

3.02331 °/min

BSTAR

-0.0089937

Orbital period

119.07 mins

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Other satellites on launch #89 in the year 1965 (1965-11-06 UTC)

EXPLORER 29 (GEOS 1), 1726

DELTA 1 DEB 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.
17 mins	2025-05-09 11:40:45.990Z	158.152° S	2025-05-09 11:48:45.990Z	106.029° ESE	25.236°	2025-05-09 11:57:45.990Z	56.87° ENE
22 mins	2025-05-09 13:41:45.990Z	219.027° SW	2025-05-09 13:51:45.990Z	351.41° N	44.959°	2025-05-09 14:03:45.990Z	40.618° NE
20 mins	2025-05-09 15:48:45.990Z	273.51° WNW	2025-05-09 15:57:45.990Z	333.51° NNW	32.765°	2025-05-09 16:08:45.990Z	39.64° NE
19 mins	2025-05-09 17:57:45.990Z	312.1° NW	2025-05-09 18:06:45.990Z	5.252° NNE	27.246°	2025-05-09 18:16:45.990Z	61.881° ENE
22 mins	2025-05-09 20:03:45.990Z	322.335° NNW	2025-05-09 20:14:45.990Z	31.408° NE	37.103°	2025-05-09 20:25:45.990Z	106.247° ESE
20 mins	2025-05-09 22:09:45.990Z	315.196° NNW	2025-05-09 22:19:45.990Z	250.161° W	42.844°	2025-05-09 22:29:45.990Z	158.768° S
10 mins	2025-05-10 00:17:45.990Z	283.161° WNW	2025-05-10 00:21:45.990Z	261.226° W	15.412°	2025-05-10 00:27:45.990Z	226.256° WSW

Authenticating...

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Check out DELTA 1 DEB, 29010 on other resources

View DELTA 1 DEB, 29010 on Heavens-Above

View DELTA 1 DEB, 29010 on Keep Track

View DELTA 1 DEB, 29010 on Celestrak

View DELTA 1 DEB, 29010 on Gunter's Space Page

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