DELTA 1 DEB, 29190

Orbit data source: Space-Track

DELTA 1 DEB, 29190 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/29190?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

29190, 1968-002P

Orbit

LEO

Country

Related business

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 shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 months ago

TLE from 2 months ago

0 DELTA 1 DEB
1 29190U 68002P   26019.82989097  .00001748  00000-0  35417-2 0  9999
2 29190 105.8407 225.2398 0277860 298.9026  58.4454 13.23155301208492

Epoch: 2026-01-19T19:55Z

TLE epoch observation values (Epoch: 2026-01-19T19:55:02.579Z)

Latitude

-0.00005°

Longitude

167.25858°

Altitude

1,069.69 km

Speed

7.368 km/s

True Right ascension

15h 00m 57s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

23:52:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,380.174 km

Perigee altitude

960.685 km

Semi-major axis

7,548.567 km

Eccentricity

0.02779

Inclination

105.8407°

RAAN

225.2398°

Arg. of periapsis

298.9026°

True anomaly

61.20777°

Mean anomaly

58.4454°

Eccentric anomaly

59.82165°

Mean motion

3.30938 °/min

Orbital period

108.78 mins

BSTAR

0.0035417

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

EXPLORER 36 (GEOS 2), 3093

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DELTA 1 DEB Visibility forecast

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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.
11 mins	2026-04-06 05:00:33.492Z	33.719° NE	2026-04-06 05:06:33.492Z	120.512° SE	37.607°	2026-04-06 05:11:33.492Z	182.673° SSW
8 mins	2026-04-06 06:48:33.492Z	353.428° N	2026-04-06 06:52:33.492Z	303.179° NW	24.51°	2026-04-06 06:56:33.492Z	255.795° W
6 mins	2026-04-06 13:42:33.492Z	68.355° E	2026-04-06 13:44:33.492Z	50.691° ENE	15.563°	2026-04-06 13:48:33.492Z	14.854° NNE
12 mins	2026-04-06 15:24:33.492Z	142.027° SSE	2026-04-06 15:30:33.492Z	53.362° ENE	43.113°	2026-04-06 15:36:33.492Z	343.328° N
10 mins	2026-04-06 17:12:33.492Z	215.058° SW	2026-04-06 17:16:33.492Z	252.267° W	22.806°	2026-04-06 17:22:33.492Z	308.752° NW

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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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out DELTA 1 DEB, 29190 on other resources

View DELTA 1 DEB, 29190 on Heavens-Above

View DELTA 1 DEB, 29190 on Keep Track

View DELTA 1 DEB, 29190 on Celestrak

View DELTA 1 DEB, 29190 on Gunter's Space Page

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

DELTA 1 DEB, 29190

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 months ago

TLE from 2 months ago

TLE epoch observation values (Epoch: 2026-01-19T19:55:02.579Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

DELTA 1 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB, 29190 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 months ago