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, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 DELTA 1 DEB
1  2700U 65089C   26136.64652436 -.00000284  00000-0 -10297-2 0  9998
2  2700  59.5978   7.6152 0723599  58.2315 337.9724 12.08990799707647

Epoch: 2026-05-16T15:30Z

TLE epoch observation values (Epoch: 2026-05-16T15:30:59.704Z)

Latitude

27.93279°

Longitude

-81.46592°

Altitude

1,111.387 km

Speed

7.538 km/s

True Right ascension

01h 42m 34s

True Declination

27° 47' 51"

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

16:06:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

2,220.427 km

Perigee altitude

1,060.012 km

Semi-major axis

8,018.357 km

Eccentricity

0.07236

Inclination

59.5978°

RAAN

7.6152°

Arg. of periapsis

58.2315°

True anomaly

334.58107°

Mean anomaly

337.9724°

Eccentric anomaly

336.30638°

Mean motion

3.02284 °/min

Orbital period

119.09 mins

BSTAR

-0.0010297

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Other satellites on launch #89 in the year 1965 (1965-11-06 UTC)

DELTA 1 DEB, 2888

DELTA 1 DEB, 27788

DELTA 1 DEB, 28662

EXPLORER 29 (GEOS 1), 1726

DELTA 1 R/B, 1729

DELTA 1 DEB, 27789

DELTA 1 DEB, 29010

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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.
12 mins	2026-05-18 17:06:43.866Z	211.165° SW	2026-05-18 17:12:43.866Z	86.059° E	43.999°	2026-05-18 17:18:43.866Z	42.232° NE
9 mins	2026-05-18 19:12:43.866Z	285.627° WNW	2026-05-18 19:16:43.866Z	332.629° NNW	23.57°	2026-05-18 19:21:43.866Z	23.828° NE
6 mins	2026-05-18 21:20:43.866Z	339.688° N	2026-05-18 21:22:43.866Z	358.713° N	14.66°	2026-05-18 21:26:43.866Z	33.894° NE
12 mins	2026-05-18 23:24:43.866Z	340.827° N	2026-05-18 23:29:43.866Z	34.314° NE	26.598°	2026-05-18 23:36:43.866Z	90.81° ESE
16 mins	2026-05-19 01:27:43.866Z	318.01° NNW	2026-05-19 01:33:43.866Z	270.494° WNW	44.6°	2026-05-19 01:43:43.866Z	147.044° SSE
9 mins	2026-05-19 03:33:43.866Z	274.363° WNW	2026-05-19 03:37:43.866Z	243.309° WSW	17.59°	2026-05-19 03:42:43.866Z	211.437° SW

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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: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-05-16T15:30:59.704Z)

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: 2 days ago