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

Last TLE update

13 hours ago

Origin

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 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Cable, 1.8 m

Radar Cross Section

3.500 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 13 hours ago

0 DELTA 1 DEB
1 02224U 66016D   25199.41304631 -.00000021  00000-0  12101-3 0  9999
2 02224 101.1320 134.7303 0137699 163.0226 317.4990 12.52159289704127

Epoch: 2025-07-18T09:54Z

TLE epoch observation values (Epoch: 2025-07-18T09:54:47.201Z)

Latitude

58.794°

Longitude

-111.57348°

Altitude

1,386.402 km

Speed

7.208 km/s

True Right ascension

22h 14m 21s

True Declination

58° 39' 13"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

50.76564°

Longitude

36.20404°

Altitude

1,498.839 km

Speed

7.103 km/s

Apparent Right ascension

03h 59m 55s

Apparent Declination

23° 39' 17"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

11:46:16

Azimuth

304.869° NW

Elevation

-3.266°

Doppler factor

Orbital elements

Apogee altitude

1,560.818 km

Perigee altitude

1,345.15 km

Semi-major axis

7,831.121 km

Eccentricity

0.01377

Inclination

101.132°

RAAN

134.7303°

Arg. of periapsis

163.0226°

True anomaly

316.41933°

Mean anomaly

317.499°

Eccentric anomaly

316.96054°

Mean motion

3.1319 °/min

Orbital period

114.95 mins

BSTAR

0.00012101

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

DELTA 1 DEB Visibility forecast

Observer location: undefined°, undefined°

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.
9 mins	2025-07-19 07:02:44.201Z	51.559° ENE	2025-07-19 07:07:44.201Z	93.388° ESE	18.056°	2025-07-19 07:11:44.201Z	127.662° SE
14 mins	2025-07-19 08:54:44.201Z	13.472° NNE	2025-07-19 09:01:44.201Z	256.146° W	44.286°	2025-07-19 09:08:44.201Z	204.645° SW
7 mins	2025-07-19 10:49:44.201Z	337.422° NNW	2025-07-19 10:52:44.201Z	312.695° NW	16.154°	2025-07-19 10:56:44.201Z	279.263° WNW
12 mins	2025-07-19 18:02:44.201Z	104.535° ESE	2025-07-19 18:07:44.201Z	59.907° ENE	26.399°	2025-07-19 18:14:44.201Z	2.539° NNE
15 mins	2025-07-19 19:52:44.201Z	175.492° S	2025-07-19 20:00:44.201Z	273.531° WNW	42.322°	2025-07-19 20:07:44.201Z	336.685° NNW

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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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

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