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

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, 0.065 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago

0 DELTA 1 DEB
1 02700U 65089C   26278.82371852  .00000169  00000-0  12398-2 0  9999
2 02700  59.5979  42.5424 0721289 147.4957 305.9125 12.08993545724837

Epoch: 2026-10-05T19:46Z

TLE epoch observation values (Epoch: 2026-10-05T19:46:09.280Z)

Latitude

59.52694°

Longitude

174.32935°

Altitude

1,339.426 km

Speed

7.332 km/s

True Right ascension

08h 21m 27s

True Declination

59° 23' 16"

Sunlit

Object was in daylight 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

12:31:01

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

2,218.562 km

Perigee altitude

1,061.853 km

Semi-major axis

8,018.345 km

Eccentricity

0.07213

Inclination

59.5979°

RAAN

42.5424°

Arg. of periapsis

147.4957°

True anomaly

298.86332°

Mean anomaly

305.9125°

Eccentric anomaly

302.42409°

Mean motion

3.02285 °/min

Orbital period

119.09 mins

BSTAR

0.0012398

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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, 2888

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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.
11 mins	2026-10-06 19:44:46.540Z	304.599° NW	2026-10-06 19:50:46.540Z	242.486° WSW	34.582°	2026-10-06 19:55:46.540Z	183.726° SSW
17 mins	2026-10-07 09:04:46.540Z	181.584° SSW	2026-10-07 09:13:46.540Z	118.334° SE	44.129°	2026-10-07 09:21:46.540Z	53.679° ENE
18 mins	2026-10-07 11:07:46.540Z	237.904° WSW	2026-10-07 11:17:46.540Z	316.45° NNW	59.482°	2026-10-07 11:25:46.540Z	33.721° NE
11 mins	2026-10-07 13:17:46.540Z	296.313° NW	2026-10-07 13:23:46.540Z	341.995° N	23.339°	2026-10-07 13:28:46.540Z	24.98° NE
8 mins	2026-10-07 15:26:46.540Z	336.442° NNW	2026-10-07 15:30:46.540Z	11.265° NNE	19.435°	2026-10-07 15:34:46.540Z	48.995° ENE
12 mins	2026-10-07 17:30:46.540Z	330.431° NNW	2026-10-07 17:36:46.540Z	43.865° NE	48.006°	2026-10-07 17:42:46.540Z	113.987° SE

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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, 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.

DELTA 1 DEB, 2700

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 23 hours ago

TLE from 23 hours ago

TLE epoch observation values (Epoch: 2026-10-05T19:46:09.280Z)

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, 2700 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 23 hours ago