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: 6 hours ago

TLE from 6 hours ago
0 DELTA 1 R/B
1  3346U 68069B   25303.87367439 -.00000018  00000-0  15759-3 0  9995
2  3346 101.5033 270.2784 0024306  85.3338 289.5903 12.54340079618888
Epoch: 2025-10-30T20:58Z
TLE epoch observation values (Epoch: 2025-10-30T20:58:05.467Z)
Latitude
14.33592°
Longitude
-86.63723°
Altitude
1,441.935 km
Speed
7.145 km/s
True Right ascension
17h 49m 14s
True Declination
14° 15' 39"
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
22:21:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,462.933 km
Perigee altitude
1,424.908 km
Semi-major axis
7,822.058 km
Eccentricity
0.00243
Inclination
101.5033°
RAAN
270.2784°
Arg. of periapsis
85.3338°
True anomaly
289.32763°
Mean anomaly
289.5903°
Eccentric anomaly
289.45899°
Mean motion
3.13734 °/min
Orbital period
114.75 mins
BSTAR
0.00015759
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