DELTA 1 DEB, 2223

Orbit data source: Space-Track

DELTA 1 DEB, 2223 is space debris in SSO originally from a launch on Mon, 28 Feb 1966 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/2223?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2223, 1966-016C

Orbit

SSO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

1 kg wet, 1 kg dry

Launch date (UTC)

1966-02-28 (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
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 DELTA 1 DEB
1 02223U 66016C   25342.66764409 -.00000006  00000-0  14648-3 0  9999
2 02223 100.7538  12.8919 0093296 260.6354 223.2861 12.87764112802430

Epoch: 2025-12-08T16:01Z

TLE epoch observation values (Epoch: 2025-12-08T16:01:24.449Z)

Latitude

55.39198°

Longitude

-109.22896°

Altitude

1,371.985 km

Speed

7.153 km/s

True Right ascension

13h 55m 08s

True Declination

55° 14' 38"

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

21:31:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,379.558 km

Perigee altitude

1,236.143 km

Semi-major axis

7,685.987 km

Eccentricity

0.00933

Inclination

100.7538°

RAAN

12.8919°

Arg. of periapsis

260.6354°

True anomaly

222.55928°

Mean anomaly

223.2861°

Eccentric anomaly

222.92207°

Mean motion

3.22102 °/min

Orbital period

111.77 mins

BSTAR

0.00014648

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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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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.
13 mins	2025-12-09 00:49:35.014Z	122.386° SE	2025-12-09 00:56:35.014Z	57.711° ENE	30.204°	2025-12-09 01:02:35.014Z	2.575° NNE
14 mins	2025-12-09 02:39:35.014Z	187.912° SSW	2025-12-09 02:45:35.014Z	249.444° W	37.707°	2025-12-09 02:53:35.014Z	333.705° NNW
13 mins	2025-12-09 14:23:35.014Z	33.079° NE	2025-12-09 14:29:35.014Z	99.139° ESE	35.53°	2025-12-09 14:36:35.014Z	169.916° S
12 mins	2025-12-09 16:13:35.014Z	356.989° N	2025-12-09 16:19:35.014Z	294.348° NW	32.053°	2025-12-09 16:25:35.014Z	236.09° WSW

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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, 2223 on other resources

View DELTA 1 DEB, 2223 on Heavens-Above

View DELTA 1 DEB, 2223 on Keep Track

View DELTA 1 DEB, 2223 on Celestrak

View DELTA 1 DEB, 2223 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, 2223

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 7 hours ago

TLE from 7 hours ago

TLE epoch observation values (Epoch: 2025-12-08T16:01:24.449Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

DELTA 1 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB, 2223 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 7 hours ago