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)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 DELTA 1 DEB
1  2223U 66016C   26036.56306348 -.00000024  00000-0  73885-4 0  9992
2  2223 100.7461  69.7537 0094136 134.4942  19.9849 12.87767591810010

Epoch: 2026-02-05T13:30Z

TLE epoch observation values (Epoch: 2026-02-05T13:30:48.684Z)

Latitude

24.70505°

Longitude

-83.67901°

Altitude

1,245.216 km

Speed

7.266 km/s

True Right ascension

16h 58m 56s

True Declination

24° 34' 59"

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

02:04:12

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,380.189 km

Perigee altitude

1,235.484 km

Semi-major axis

7,685.973 km

Eccentricity

0.00941

Inclination

100.7461°

RAAN

69.7537°

Arg. of periapsis

134.4942°

True anomaly

20.35769°

Mean anomaly

19.9849°

Eccentric anomaly

20.17088°

Mean motion

3.22103 °/min

Orbital period

111.77 mins

BSTAR

0.000073885

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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.
11 mins	2026-02-07 00:18:10.323Z	104.754° ESE	2026-02-07 00:24:10.323Z	52.85° ENE	21.41°	2026-02-07 00:29:10.323Z	9.902° NNE
13 mins	2026-02-07 02:07:10.323Z	170.873° S	2026-02-07 02:13:10.323Z	263.627° W	44.108°	2026-02-07 02:20:10.323Z	340.392° N
10 mins	2026-02-07 13:51:10.323Z	48.758° ENE	2026-02-07 13:55:10.323Z	89.522° E	24.42°	2026-02-07 14:01:10.323Z	148.617° SSE
12 mins	2026-02-07 15:40:10.323Z	4.691° NNE	2026-02-07 15:46:10.323Z	285.098° WNW	39.597°	2026-02-07 15:52:10.323Z	218.981° 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, 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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-02-05T13:30:48.684Z)

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: 1 day ago