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

16 hours 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 16 hours ago

0 DELTA 1 DEB
1 02700U 65089C   25128.59234006  .00000242  00000-0  16159-2 0  9996
2 02700  59.5941 140.3108 0718437 181.8514 284.4730 12.08966132662537

Epoch: 2025-05-08T14:12Z

Definitive object data (Epoch: 2025-05-08T14:12:58.181Z)

Latitude

58.73331°

Longitude

166.31062°

Altitude

1,545.276 km

Speed

7.146 km/s

True Right ascension

16h 24m 51s

True Declination

58° 35' 45"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

20.39242°

Longitude

-133.66684°

Altitude

1,116.918 km

Speed

7.531 km/s

Apparent Right ascension

22h 46m 48s

Apparent Declination

-9° 54' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:32:10

Azimuth

75.085° E

Elevation

-31.944°

Doppler factor

Orbital elements

Apogee altitude

2,216.406 km

Perigee altitude

1,064.253 km

Semi-major axis

8,018.466 km

Eccentricity

0.0718437

Inclination

59.5941°

RAAN

140.3108°

Arg. of periapsis

181.8514°

True anomaly

276.34614°

Mean anomaly

284.473°

Eccentric anomaly

280.4246°

Mean motion

3.02278 °/min

BSTAR

0.0016159

Orbital period

119.1 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.
13 mins	2025-05-09 07:58:21.338Z	320.462° NNW	2025-05-09 08:05:21.338Z	6.704° NNE	22.163°	2025-05-09 08:11:21.338Z	57.109° ENE
13 mins	2025-05-09 10:05:21.338Z	328.776° NNW	2025-05-09 10:12:21.338Z	45.105° ENE	38.122°	2025-05-09 10:18:21.338Z	113.143° SE
12 mins	2025-05-09 12:09:21.338Z	304.303° NW	2025-05-09 12:15:21.338Z	247.962° W	30.854°	2025-05-09 12:21:21.338Z	181.848° SSW
20 mins	2025-05-10 01:26:21.338Z	181.826° SSW	2025-05-10 01:36:21.338Z	118.075° SE	36.275°	2025-05-10 01:46:21.338Z	50.443° ENE
21 mins	2025-05-10 03:29:21.338Z	236.41° WSW	2025-05-10 03:40:21.338Z	307.583° NW	41.766°	2025-05-10 03:50:21.338Z	35.579° NE
15 mins	2025-05-10 05:39:21.338Z	289.939° WNW	2025-05-10 05:47:21.338Z	341.913° N	25.448°	2025-05-10 05:54:21.338Z	33.48° NE

Authenticating...

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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

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