DELTA 1 R/B, 3315

Orbit data source: Space-Track

DELTA 1 R/B, 3315 is space debris originally from a launch on Thu, 04 Jul 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
3315, 1968-055B
Orbit
Active
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 37, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
1968-07-04 (57 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere + Cone, 0.5 m
Radar Cross Section
0.734 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 DELTA 1 R/B
1 03315U 68055B   25258.53339174  .00000113  00000-0  33778-3 0  9999
2 03315 120.6595 198.1522 2639034 135.0662 332.6933  9.25691675916128
Epoch: 2025-09-15T12:48Z
TLE epoch observation values (Epoch: 2025-09-15T12:48:05.046Z)
Latitude
59.44555°
Longitude
-75.95121°
Altitude
1,172.169 km
Speed
8.011 km/s
True Right ascension
07h 23m 13s
True Declination
59° 18' 11"
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
17:53:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,730.992 km
Perigee altitude
674.212 km
Semi-major axis
9,580.739 km
Eccentricity
0.2639
Inclination
120.6595°
RAAN
198.1522°
Arg. of periapsis
135.0662°
True anomaly
313.57243°
Mean anomaly
332.6933°
Eccentric anomaly
323.75301°
Mean motion
2.31443 °/min
Orbital period
155.55 mins
BSTAR
0.00033778
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