DELTA 1 DEB, 29187

Orbit data source: Space-Track

DELTA 1 DEB, 29187 is space debris in LEO originally from a launch on Thu, 11 Jan 1968 UTC launched from the Air Force Western Test Range (AFWTR). 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/29187?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29187, 1968-002L

Orbit

LEO

Last TLE update

3 days ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1968-01-11 (58 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 3 days ago

0 DELTA 1 DEB
1 29187U 68002L   25197.24417818  .00000092  00000-0  52190-3 0  9993
2 29187 105.8071 181.2386 0296562  56.9454 323.9005 12.91156156558752

Epoch: 2025-07-16T05:51Z

TLE epoch observation values (Epoch: 2025-07-16T05:51:36.994Z)

Latitude

18.04621°

Longitude

153.74217°

Altitude

1,117.332 km

Speed

7.381 km/s

True Right ascension

11h 43m 53s

True Declination

17° 57' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

18.59995°

Longitude

-11.65792°

Altitude

1,363.828 km

Speed

7.148 km/s

Apparent Right ascension

00h 35m 56s

Apparent Declination

-7° 31' 08"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:26:26

Azimuth

355.605° N

Elevation

-57.533°

Doppler factor

Orbital elements

Apogee altitude

1,522.258 km

Perigee altitude

1,067.163 km

Semi-major axis

7,672.847 km

Eccentricity

0.02966

Inclination

105.8071°

RAAN

181.2386°

Arg. of periapsis

56.9454°

True anomaly

321.83693°

Mean anomaly

323.9005°

Eccentric anomaly

322.87495°

Mean motion

3.2293 °/min

Orbital period

111.48 mins

BSTAR

0.0005219

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Other satellites on launch #2 in the year 1968 (1968-01-11 UTC)

EXPLORER 36 (GEOS 2), 3093

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.
9 mins	2025-07-19 10:38:47.457Z	61.813° ENE	2025-07-19 10:42:47.457Z	96.593° ESE	17.282°	2025-07-19 10:47:47.457Z	138.458° SSE
13 mins	2025-07-19 12:26:47.457Z	21.367° NNE	2025-07-19 12:32:47.457Z	263.855° W	44.883°	2025-07-19 12:39:47.457Z	207.263° SW
7 mins	2025-07-19 14:17:47.457Z	341.73° N	2025-07-19 14:20:47.457Z	312.276° NW	18.238°	2025-07-19 14:24:47.457Z	276.095° WNW
9 mins	2025-07-19 21:19:47.457Z	103.249° ESE	2025-07-19 21:23:47.457Z	57.885° ENE	25.018°	2025-07-19 21:28:47.457Z	1.178° NNE
11 mins	2025-07-19 23:07:47.457Z	178.956° S	2025-07-19 23:12:47.457Z	249.664° W	38.595°	2025-07-19 23:18:47.457Z	326.907° NNW

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Check out DELTA 1 DEB, 29187 on other resources

View DELTA 1 DEB, 29187 on Heavens-Above

View DELTA 1 DEB, 29187 on Keep Track

View DELTA 1 DEB, 29187 on Celestrak

View DELTA 1 DEB, 29187 on Gunter's Space Page

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