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 (61 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

DISK + CABLE, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 DELTA 1 DEB
1 02223U 66016C   26255.00667898 -.00000014  00000-0  11165-3 0  9995
2 02223 100.7254 280.3846 0093946  27.0138  40.0423 12.87776911838138

Epoch: 2026-09-12T00:09Z

TLE epoch observation values (Epoch: 2026-09-12T00:09:37.063Z)

Latitude

65.50786°

Longitude

-97.47816°

Altitude

1,266.523 km

Speed

7.254 km/s

True Right ascension

17h 03m 47s

True Declination

65° 23' 11"

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

06:41:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,380.004 km

Perigee altitude

1,235.592 km

Semi-major axis

7,685.935 km

Eccentricity

0.00939

Inclination

100.7254°

RAAN

280.3846°

Arg. of periapsis

27.0138°

True anomaly

40.74116°

Mean anomaly

40.0423°

Eccentric anomaly

40.3911°

Mean motion

3.22105 °/min

Orbital period

111.76 mins

BSTAR

0.00011165

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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.
14 mins	2026-09-12 15:19:21.277Z	6.953° NNE	2026-09-12 15:26:21.277Z	284.109° WNW	58.434°	2026-09-12 15:33:21.277Z	216.656° SW
10 mins	2026-09-13 00:13:21.277Z	103.173° ESE	2026-09-13 00:17:21.277Z	62.993° ENE	26.514°	2026-09-13 00:23:21.277Z	6.658° NNE
13 mins	2026-09-13 02:01:21.277Z	179.504° S	2026-09-13 02:07:21.277Z	264.852° W	62.056°	2026-09-13 02:14:21.277Z	337.316° NNW
12 mins	2026-09-13 13:44:21.277Z	38.897° NE	2026-09-13 13:50:21.277Z	102.152° ESE	35.785°	2026-09-13 13:56:21.277Z	158.538° S

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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: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-09-12T00:09:37.063Z)

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: 14 hours ago