DELTA 1 DEB, 2224

Orbit data source: Space-Track

DELTA 1 DEB, 2224 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/2224?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2224, 1966-016D

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: 3 days ago

TLE from 3 days ago

0 DELTA 1 DEB
1  2224U 66016D   26037.27807223 -.00000011  00000-0  17998-3 0  9998
2  2224 101.1515 324.8653 0138062 122.6100  31.4776 12.52169960729512

Epoch: 2026-02-06T06:40Z

TLE epoch observation values (Epoch: 2026-02-06T06:40:25.440Z)

Latitude

24.59602°

Longitude

-86.50768°

Altitude

1,366.294 km

Speed

7.22 km/s

True Right ascension

10h 00m 03s

True Declination

24° 28' 35"

Sunlit

Object was in full shadow 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

21:57:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,561.058 km

Perigee altitude

1,344.823 km

Semi-major axis

7,831.078 km

Eccentricity

0.01381

Inclination

101.1515°

RAAN

324.8653°

Arg. of periapsis

122.61°

True anomaly

32.31601°

Mean anomaly

31.4776°

Eccentric anomaly

31.89556°

Mean motion

3.13192 °/min

Orbital period

114.95 mins

BSTAR

0.00017998

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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	2026-02-09 07:20:43.703Z	27.775° NE	2026-02-09 07:27:43.703Z	93.957° ESE	37.021°	2026-02-09 07:34:43.703Z	172.234° S
11 mins	2026-02-09 09:15:43.703Z	352.699° N	2026-02-09 09:20:43.703Z	300.2° NW	29.892°	2026-02-09 09:26:43.703Z	241.472° WSW
5 mins	2026-02-09 16:33:43.703Z	66.069° ENE	2026-02-09 16:35:43.703Z	50.722° ENE	12.99°	2026-02-09 16:38:43.703Z	27.432° NE
14 mins	2026-02-09 18:20:43.703Z	143.913° SSE	2026-02-09 18:27:43.703Z	60.948° ENE	41.698°	2026-02-09 18:34:43.703Z	350.795° N

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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, 2224 on other resources

View DELTA 1 DEB, 2224 on Heavens-Above

View DELTA 1 DEB, 2224 on Keep Track

View DELTA 1 DEB, 2224 on Celestrak

View DELTA 1 DEB, 2224 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, 2224

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-02-06T06:40:25.440Z)

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, 2224 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago