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: 15 hours ago

TLE from 15 hours ago
0 DELTA 1 R/B
1 03346U 68069B   26042.50049106 -.00000024  00000-0  12338-3 0  9991
2 03346 101.5212  10.9511 0023573 243.0982 229.9269 12.54342770631874
Epoch: 2026-02-11T12:00Z
TLE epoch observation values (Epoch: 2026-02-11T12:00:42.427Z)
Latitude
64.66198°
Longitude
-105.42723°
Altitude
1,469.272 km
Speed
7.129 km/s
True Right ascension
14h 25m 15s
True Declination
64° 32' 27"
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
04:59:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,462.349 km
Perigee altitude
1,425.472 km
Semi-major axis
7,822.048 km
Eccentricity
0.00236
Inclination
101.5212°
RAAN
10.9511°
Arg. of periapsis
243.0982°
True anomaly
229.72058°
Mean anomaly
229.9269°
Eccentric anomaly
229.8237°
Mean motion
3.13735 °/min
Orbital period
114.75 mins
BSTAR
0.00012338
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