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
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 DELTA 1 R/B
1  3346U 68069B   26132.85276855 -.00000042  00000-0  13492-4 0  9995
2  3346 101.5357  98.8689 0024388  67.3319 347.7278 12.54344902643209
Epoch: 2026-05-12T20:27Z
TLE epoch observation values (Epoch: 2026-05-12T20:27:59.202Z)
Latitude
53.4746°
Longitude
-94.66409°
Altitude
1,436.281 km
Speed
7.157 km/s
True Right ascension
05h 31m 48s
True Declination
53° 19' 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
10:40:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,462.979 km
Perigee altitude
1,424.826 km
Semi-major axis
7,822.039 km
Eccentricity
0.00244
Inclination
101.5357°
RAAN
98.8689°
Arg. of periapsis
67.3319°
True anomaly
347.66822°
Mean anomaly
347.7278°
Eccentric anomaly
347.69803°
Mean motion
3.13735 °/min
Orbital period
114.75 mins
BSTAR
0.000013492
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