DELTA 1 R/B, 3346

Orbit data source: Space-Track

DELTA 1 R/B, 3346 is space debris in SSO originally from a launch on Fri, 16 Aug 1968 UTC launched from the Air Force Western Test Range (AFWTR). 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
3346, 1968-069B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Aerojet
Mission
Spacecraft
Bus & Motor
ABLESTAR, Unknown motor
Mass
~785 kg wet, ~785 kg dry
Launch date (UTC)
1968-08-16 (57 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 DELTA 1 R/B
1  3346U 68069B   25317.82977108 -.00000006  00000-0  23127-3 0  9990
2  3346 101.5061 283.8291 0024277  58.4651 309.7204 12.54340609620632
Epoch: 2025-11-13T19:54Z
TLE epoch observation values (Epoch: 2025-11-13T19:54:52.221Z)
Latitude
7.74861°
Longitude
-69.64988°
Altitude
1,436.198 km
Speed
7.149 km/s
True Right ascension
18h 48m 59s
True Declination
7° 42' 24"
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
21:47:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,462.908 km
Perigee altitude
1,424.929 km
Semi-major axis
7,822.056 km
Eccentricity
0.00243
Inclination
101.5061°
RAAN
283.8291°
Arg. of periapsis
58.4651°
True anomaly
309.50601°
Mean anomaly
309.7204°
Eccentric anomaly
309.61324°
Mean motion
3.13734 °/min
Orbital period
114.75 mins
BSTAR
0.00023127
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