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 (58 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 R/B
1 03346U 68069B   26312.13740987 -.00000044  00000-0 -12689-5 0  9999
2 03346 101.5622 273.5865 0024270  77.5636 294.3122 12.54347953665687
Epoch: 2026-11-08T03:17Z
TLE epoch observation values (Epoch: 2026-11-08T03:17:52.212Z)
Latitude
11.34197°
Longitude
174.44608°
Altitude
1,440.416 km
Speed
7.146 km/s
True Right ascension
18h 04m 59s
True Declination
11° 16' 54"
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
23:15:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,462.875 km
Perigee altitude
1,424.907 km
Semi-major axis
7,822.028 km
Eccentricity
0.00243
Inclination
101.5622°
RAAN
273.5865°
Arg. of periapsis
77.5636°
True anomaly
294.05843°
Mean anomaly
294.3122°
Eccentric anomaly
294.18535°
Mean motion
3.13736 °/min
Orbital period
114.75 mins
BSTAR
-0.0000012689
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