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

4 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 4 days ago

0 DELTA 1 DEB
1 02700U 65089C   25184.26839412  .00000221  00000-0  15109-2 0  9995
2 02700  59.5968  13.0534 0715435 217.1314 322.6797 12.08968141669268

Epoch: 2025-07-03T06:26Z

TLE epoch observation values (Epoch: 2025-07-03T06:26:29.251Z)

Latitude

4.71388°

Longitude

172.13483°

Altitude

1,202.022 km

Speed

7.45 km/s

True Right ascension

12h 41m 10s

True Declination

4° 41' 15"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-46.66544°

Longitude

-51.71766°

Altitude

1,550.808 km

Speed

7.139 km/s

Apparent Right ascension

22h 04m 11s

Apparent Declination

-43° 35' 24"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

10:24:41

Azimuth

135.542° SSE

Elevation

-84.7°

Doppler factor

Orbital elements

Apogee altitude

2,213.989 km

Perigee altitude

1,066.652 km

Semi-major axis

8,018.457 km

Eccentricity

0.07154

Inclination

59.5968°

RAAN

13.0534°

Arg. of periapsis

217.1314°

True anomaly

Unknown

Mean anomaly

322.6797°

Eccentric anomaly

Unknown

Mean motion

3.02278 °/min

Orbital period

119.1 mins

BSTAR

0.0015109

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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.
15 mins	2025-07-06 23:26:33.667Z	308.232° NW	2025-07-06 23:34:33.667Z	249.7° W	32.831°	2025-07-06 23:41:33.667Z	182.339° SSW
22 mins	2025-07-07 12:42:33.667Z	183.406° SSW	2025-07-07 12:53:33.667Z	112.042° ESE	37.205°	2025-07-07 13:04:33.667Z	48.281° ENE
23 mins	2025-07-07 14:46:33.667Z	237.897° WSW	2025-07-07 14:57:33.667Z	313.705° NW	42.043°	2025-07-07 15:09:33.667Z	37.817° NE
19 mins	2025-07-07 16:55:33.667Z	287.844° WNW	2025-07-07 17:04:33.667Z	339.656° N	27.997°	2025-07-07 17:14:33.667Z	41.99° NE
17 mins	2025-07-07 19:04:33.667Z	318.77° NNW	2025-07-07 19:13:33.667Z	13.3° NNE	26.408°	2025-07-07 19:21:33.667Z	69.014° E
18 mins	2025-07-07 21:10:33.667Z	323.619° NNW	2025-07-07 21:20:33.667Z	45.561° ENE	40.936°	2025-07-07 21:28:33.667Z	120.075° SE

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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.