DELTA 1 DEB, 2700

Orbit data source: Space-Track

DELTA 1 DEB, 2700 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/2700?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2700, 1965-089C

Orbit

LEO

Last TLE update

2 days 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 2 days ago

0 DELTA 1 DEB
1 02700U 65089C   25171.36788444 -.00000183  00000-0 -54537-3 0  9998
2 02700  59.5997  42.5393 0716074 208.9713 336.1368 12.08965013667707

Epoch: 2025-06-20T08:49Z

TLE epoch observation values (Epoch: 2025-06-20T08:49:45.215Z)

Latitude

-1.37974°

Longitude

-177.91583°

Altitude

1,124.812 km

Speed

7.522 km/s

True Right ascension

14h 53m 22s

True Declination

-1° 22' 19"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

25.46577°

Longitude

160.04906°

Altitude

1,327.334 km

Speed

7.336 km/s

Apparent Right ascension

13h 22m 54s

Apparent Declination

-3° 44' 11"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

01:19:35

Azimuth

358.599° N

Elevation

-53.812°

Doppler factor

Orbital elements

Apogee altitude

2,214.516 km

Perigee altitude

1,066.152 km

Semi-major axis

8,018.471 km

Eccentricity

0.07161

Inclination

59.5997°

RAAN

42.5393°

Arg. of periapsis

208.9713°

True anomaly

Unknown

Mean anomaly

336.1368°

Eccentric anomaly

Unknown

Mean motion

3.02278 °/min

Orbital period

119.1 mins

BSTAR

-0.00054537

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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.
21 mins	2025-06-22 15:24:59.774Z	171.492° S	2025-06-22 15:35:59.774Z	111.912° ESE	30.371°	2025-06-22 15:45:59.774Z	54.702° ENE
23 mins	2025-06-22 17:27:59.774Z	223.821° SW	2025-06-22 17:39:59.774Z	321.693° NNW	44.547°	2025-06-22 17:50:59.774Z	38.651° NE
20 mins	2025-06-22 19:35:59.774Z	274.435° WNW	2025-06-22 19:45:59.774Z	332.81° NNW	30.579°	2025-06-22 19:55:59.774Z	37.937° NE
16 mins	2025-06-22 21:45:59.774Z	313.506° NW	2025-06-22 21:53:59.774Z	359.961° N	24.307°	2025-06-22 22:01:59.774Z	56.25° ENE
17 mins	2025-06-22 23:52:59.774Z	325.708° NNW	2025-06-23 00:01:59.774Z	34.608° NE	35.534°	2025-06-23 00:09:59.774Z	105.517° ESE
15 mins	2025-06-23 01:57:59.774Z	313.116° NW	2025-06-23 02:05:59.774Z	249.112° W	39.847°	2025-06-23 02:12:59.774Z	166.393° S

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Check out DELTA 1 DEB, 2700 on other resources

View DELTA 1 DEB, 2700 on Heavens-Above

View DELTA 1 DEB, 2700 on Keep Track

View DELTA 1 DEB, 2700 on Celestrak

View DELTA 1 DEB, 2700 on Gunter's Space Page

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