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: 9 hours ago

TLE from 9 hours ago

0 DELTA 1 DEB
1  2224U 66016D   26119.70304707 -.00000039  00000-0  15897-4 0  9993
2  2224 101.1554  42.1928 0137626 320.2999  67.9777 12.52173425739839

Epoch: 2026-04-29T16:52Z

TLE epoch observation values (Epoch: 2026-04-29T16:52:23.266Z)

Latitude

29.17799°

Longitude

-74.85465°

Altitude

1,419.631 km

Speed

7.171 km/s

True Right ascension

02h 23m 36s

True Declination

29° 02' 39"

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

09:32:06

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,560.702 km

Perigee altitude

1,345.151 km

Semi-major axis

7,831.063 km

Eccentricity

0.01376

Inclination

101.1554°

RAAN

42.1928°

Arg. of periapsis

320.2999°

True anomaly

69.44904°

Mean anomaly

67.9777°

Eccentric anomaly

68.71244°

Mean motion

3.13193 °/min

Orbital period

114.95 mins

BSTAR

0.000015897

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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.
15 mins	2026-04-30 06:46:26.100Z	32.295° NE	2026-04-30 06:54:26.100Z	103.763° ESE	33.034°	2026-04-30 07:01:26.100Z	163.262° S
14 mins	2026-04-30 08:40:26.100Z	1.984° NNE	2026-04-30 08:47:26.100Z	288.408° WNW	36.914°	2026-04-30 08:54:26.100Z	227.888° WSW
14 mins	2026-04-30 17:46:26.100Z	130.827° SE	2026-04-30 17:52:26.100Z	68.713° E	36.936°	2026-04-30 18:00:26.100Z	353.856° N
12 mins	2026-04-30 19:40:26.100Z	206.718° SW	2026-04-30 19:45:26.100Z	257.973° W	30.919°	2026-04-30 19:52:26.100Z	324.377° NNW

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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: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-04-29T16:52:23.266Z)

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: 9 hours ago