DELTA 1 DEB, 6214

Orbit data source: Space-Track

DELTA 1 DEB, 6214 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/6214?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

6214, 1966-016E

Orbit

SSO

Last TLE update

13 hours ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

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

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 13 hours ago

0 DELTA 1 DEB
1  6214U 66016E   25222.23937315  .00000072  00000-0  63698-3 0  9992
2  6214 101.7423 214.4225 0121181  52.7142 328.5593 12.62714346735914

Epoch: 2025-08-10T05:44Z

TLE epoch observation values (Epoch: 2025-08-10T05:44:41.84Z)

Latitude

20.09709°

Longitude

164.94464°

Altitude

1,333.736 km

Speed

7.229 km/s

True Right ascension

14h 00m 19s

True Declination

19° 59' 41"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-60.23443°

Longitude

-168.97282°

Altitude

1,472.114 km

Speed

7.109 km/s

Apparent Right ascension

18h 40m 24s

Apparent Declination

-57° 36' 04"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

08:54:45

Azimuth

140.626° SSE

Elevation

-62.146°

Doppler factor

Orbital elements

Apogee altitude

1,503.659 km

Perigee altitude

1,314.921 km

Semi-major axis

7,787.427 km

Eccentricity

0.01212

Inclination

101.7423°

RAAN

214.4225°

Arg. of periapsis

52.7142°

True anomaly

327.82551°

Mean anomaly

328.5593°

Eccentric anomaly

328.19336°

Mean motion

3.15829 °/min

Orbital period

113.99 mins

BSTAR

0.00063698

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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.
5 mins	2025-08-10 21:05:15.351Z	68.002° E	2025-08-10 21:08:15.351Z	43.444° NE	13.008°	2025-08-10 21:10:15.351Z	27.316° NE
13 mins	2025-08-10 22:52:15.351Z	144.721° SSE	2025-08-10 22:58:15.351Z	70.064° E	42.28°	2025-08-10 23:05:15.351Z	349.182° N
10 mins	2025-08-11 00:46:15.351Z	221.875° SW	2025-08-11 00:51:15.351Z	270.019° WNW	22.111°	2025-08-11 00:56:15.351Z	313.715° NW
9 mins	2025-08-11 10:50:15.351Z	59.695° ENE	2025-08-11 10:54:15.351Z	93.192° ESE	17.631°	2025-08-11 10:59:15.351Z	132.242° SE
14 mins	2025-08-11 12:40:15.351Z	16.03° NNE	2025-08-11 12:47:15.351Z	237.498° WSW	44.755°	2025-08-11 12:54:15.351Z	202.33° SSW
8 mins	2025-08-11 14:34:15.351Z	338.912° N	2025-08-11 14:38:15.351Z	303.959° NW	18.207°	2025-08-11 14:42:15.351Z	271.814° WNW

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, 6214 on other resources

View DELTA 1 DEB, 6214 on Heavens-Above

View DELTA 1 DEB, 6214 on Keep Track

View DELTA 1 DEB, 6214 on Celestrak

View DELTA 1 DEB, 6214 on Gunter's Space Page

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