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

6 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 6 days ago

0 DELTA 1 DEB
1 02700U 65089C   25176.32920044  .00000017  00000-0  47142-3 0  9991
2 02700  59.6001  31.2002 0715702 212.0898 329.1380 12.08965024668308

Epoch: 2025-06-25T07:54Z

TLE epoch observation values (Epoch: 2025-06-25T07:54:02.918Z)

Latitude

2.80034°

Longitude

177.33969°

Altitude

1,161.213 km

Speed

7.488 km/s

True Right ascension

13h 58m 15s

True Declination

2° 47' 04"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-19.51666°

Longitude

-26.8449°

Altitude

1,915.652 km

Speed

6.816 km/s

Apparent Right ascension

02h 56m 01s

Apparent Declination

-50° 10' 21"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:15:25

Azimuth

134.347° SE

Elevation

-26.823°

Doppler factor

Orbital elements

Apogee altitude

2,214.217 km

Perigee altitude

1,066.45 km

Semi-major axis

8,018.471 km

Eccentricity

0.07157

Inclination

59.6001°

RAAN

31.2002°

Arg. of periapsis

212.0898°

True anomaly

Unknown

Mean anomaly

329.138°

Eccentric anomaly

Unknown

Mean motion

3.02278 °/min

Orbital period

119.1 mins

BSTAR

0.00047142

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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.
22 mins	2025-07-01 13:47:06.887Z	179.39° S	2025-07-01 13:58:06.887Z	116.791° SE	34.633°	2025-07-01 14:09:06.887Z	50.745° ENE
23 mins	2025-07-01 15:51:06.887Z	232.196° WSW	2025-07-01 16:02:06.887Z	302.627° NW	43.192°	2025-07-01 16:14:06.887Z	37.854° NE
19 mins	2025-07-01 18:00:06.887Z	283.764° WNW	2025-07-01 18:09:06.887Z	336.677° NNW	28.901°	2025-07-01 18:19:06.887Z	40.084° NE
17 mins	2025-07-01 20:09:06.887Z	316.656° NNW	2025-07-01 20:18:06.887Z	10.884° NNE	25.427°	2025-07-01 20:26:06.887Z	65.351° ENE
17 mins	2025-07-01 22:16:06.887Z	325.651° NNW	2025-07-01 22:25:06.887Z	39.405° NE	38.887°	2025-07-01 22:33:06.887Z	113.974° SE
15 mins	2025-07-02 00:21:06.887Z	308.908° NW	2025-07-02 00:29:06.887Z	241.427° WSW	35.503°	2025-07-02 00:36:06.887Z	175.318° 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

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