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

20 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 20 hours ago

0 DELTA 1 DEB
1  6214U 66016E   25181.91363059  .00000090  00000-0  73278-3 0  9994
2  6214 101.7383 173.8326 0120407 131.0846 258.4695 12.62703424730825

Epoch: 2025-06-30T21:55Z

TLE epoch observation values (Epoch: 2025-06-30T21:55:37.682Z)

Latitude

27.60541°

Longitude

-80.49789°

Altitude

1,434.743 km

Speed

7.137 km/s

True Right ascension

11h 10m 30s

True Declination

27° 28' 36"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-63.77038°

Longitude

81.7402°

Altitude

1,477.345 km

Speed

7.105 km/s

Apparent Right ascension

19h 27m 55s

Apparent Declination

-57° 10' 59"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

05:44:29

Azimuth

215.478° SW

Elevation

-65.967°

Doppler factor

Orbital elements

Apogee altitude

1,503.101 km

Perigee altitude

1,315.568 km

Semi-major axis

7,787.472 km

Eccentricity

0.01204

Inclination

101.7383°

RAAN

173.8326°

Arg. of periapsis

131.0846°

True anomaly

Unknown

Mean anomaly

258.4695°

Eccentric anomaly

Unknown

Mean motion

3.15826 °/min

Orbital period

113.99 mins

BSTAR

0.00073278

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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	2025-07-01 20:50:47.705Z	64.659° ENE	2025-07-01 20:52:47.705Z	49.768° ENE	11.771°	2025-07-01 20:55:47.705Z	26.911° NE
14 mins	2025-07-01 22:36:47.705Z	139.097° SSE	2025-07-01 22:43:47.705Z	61.104° ENE	39.993°	2025-07-01 22:50:47.705Z	351.669° N
11 mins	2025-07-02 00:30:47.705Z	213.341° SW	2025-07-02 00:35:47.705Z	261.85° W	27.078°	2025-07-02 00:41:47.705Z	317.703° NNW
5 mins	2025-07-02 10:36:47.705Z	70.764° E	2025-07-02 10:38:47.705Z	87.131° E	13.149°	2025-07-02 10:41:47.705Z	111.702° ESE
14 mins	2025-07-02 12:25:47.705Z	19.68° NNE	2025-07-02 12:31:47.705Z	62.664° ENE	44.53°	2025-07-02 12:39:47.705Z	195.808° SSW
8 mins	2025-07-02 14:19:47.705Z	339.337° N	2025-07-02 14:22:47.705Z	311.661° NW	19.812°	2025-07-02 14:27:47.705Z	266.504° W

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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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