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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Identifier
6214, 1966-016E
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
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: 1 day ago

TLE from 1 day ago
0 DELTA 1 DEB
1 06214U 66016E   25241.44246419  .00000085  00000-0  70901-3 0  9993
2 06214 101.7452 233.7571 0120768  15.3672 141.2439 12.62719024738096
Epoch: 2025-08-29T10:37Z
TLE epoch observation values (Epoch: 2025-08-29T10:37:08.906Z)
Latitude
22.05056°
Longitude
-78.61379°
Altitude
1,487.952 km
Speed
7.088 km/s
True Right ascension
03h 54m 15s
True Declination
21° 56' 32"
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
05:44:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,503.318 km
Perigee altitude
1,315.224 km
Semi-major axis
7,787.408 km
Eccentricity
0.01208
Inclination
101.7452°
RAAN
233.7571°
Arg. of periapsis
15.3672°
True anomaly
142.10011°
Mean anomaly
141.2439°
Eccentric anomaly
141.67301°
Mean motion
3.1583 °/min
Orbital period
113.99 mins
BSTAR
0.00070901
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Other satellites on launch #16 in the year 1966 (1966-02-28 UTC)

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