DELTA 1 DEB, 2888

Orbit data source: Space-Track

DELTA 1 DEB, 2888 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/2888?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2888, 1965-089D

Orbit

LEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1965-11-06 (61 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

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: 3 days ago

TLE from 3 days ago

0 DELTA 1 DEB
1 02888U 65089D   26133.27823083 -.00000119  00000-0 -33832-3 0  9997
2 02888  59.2047  70.4821 0715927 231.3026 293.0696 11.87428380570341

Epoch: 2026-05-13T06:40Z

TLE epoch observation values (Epoch: 2026-05-13T06:40:39.143Z)

Latitude

19.99638°

Longitude

-93.18562°

Altitude

1,547.529 km

Speed

7.178 km/s

True Right ascension

15h 52m 04s

True Declination

19° 53' 50"

Sunlit

Object was in full shadow 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

14:04:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

2,318.052 km

Perigee altitude

1,156.074 km

Semi-major axis

8,115.2 km

Eccentricity

0.07159

Inclination

59.2047°

RAAN

70.4821°

Arg. of periapsis

231.3026°

True anomaly

285.27211°

Mean anomaly

293.0696°

Eccentric anomaly

289.19571°

Mean motion

2.96889 °/min

Orbital period

121.26 mins

BSTAR

-0.00033832

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

EXPLORER 29 (GEOS 1), 1726

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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.
17 mins	2026-05-16 07:11:13.135Z	306.505° NW	2026-05-16 07:20:13.135Z	252.805° W	28.077°	2026-05-16 07:28:13.135Z	191.551° SSW
14 mins	2026-05-16 18:42:13.135Z	135.441° SSE	2026-05-16 18:49:13.135Z	100.046° ESE	17.549°	2026-05-16 18:56:13.135Z	67.345° ENE
24 mins	2026-05-16 20:42:13.135Z	200.443° SSW	2026-05-16 20:53:13.135Z	128.251° SE	43.036°	2026-05-16 21:06:13.135Z	43.828° NE
23 mins	2026-05-16 22:50:13.135Z	254.392° W	2026-05-16 23:01:13.135Z	324.062° NNW	38.094°	2026-05-16 23:13:13.135Z	38.613° NE
20 mins	2026-05-17 01:02:13.135Z	299.73° NW	2026-05-17 01:12:13.135Z	355.574° N	27.625°	2026-05-17 01:22:13.135Z	52.76° ENE
19 mins	2026-05-17 03:13:13.135Z	322.723° NNW	2026-05-17 03:23:13.135Z	26.444° NE	32.527°	2026-05-17 03:32:13.135Z	89.39° E
9 mins	2026-05-17 05:20:13.135Z	318.873° NNW	2026-05-17 05:29:13.135Z	316.983° NNW	42.286°	2026-05-17 05:29:13.135Z	316.983° NNW

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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, 2888 on other resources

View DELTA 1 DEB, 2888 on Heavens-Above

View DELTA 1 DEB, 2888 on Keep Track

View DELTA 1 DEB, 2888 on Celestrak

View DELTA 1 DEB, 2888 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, 2888

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-05-13T06:40:39.143Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

DELTA 1 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB, 2888 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago