ATLAS D R/B, 1616

Orbit data source: Space-Track

ATLAS D R/B, 1616 is space debris in LEO originally from a launch on Tue, 05 Oct 1965 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
1616, 1965-078B
Orbit
LEO
Last TLE update
10 hours ago
Origin
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
70 kg wet, 70 kg dry
Launch date (UTC)
1965-10-05 (60 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.6 m
Radar Cross Section
8.765 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 10 hours ago
0 ATLAS D R/B
1 01616U 65078B   25199.59095511  .00004077  00000-0  32969-3 0  9991
2 01616 144.2308 145.7169 0988216 121.6204 248.4636 13.32671709706107
Epoch: 2025-07-18T14:10Z
TLE epoch observation values (Epoch: 2025-07-18T14:10:58.521Z)
Latitude
Longitude
-3.66716°
Altitude
1,468.142 km
Speed
6.971 km/s
True Right ascension
09h 42m 52s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
31.54819°
Longitude
-123.8926°
Altitude
399.307 km
Speed
8.043 km/s
Apparent Right ascension
01h 09m 14s
Apparent Declination
-2° 57' 07"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:30:34
Azimuth
344.191° N
Elevation
-52.012°
Doppler factor
1
Orbital elements
Apogee altitude
1,882.523 km
Perigee altitude
396.692 km
Semi-major axis
7,517.745 km
Eccentricity
0.09882
Inclination
144.2308°
RAAN
145.7169°
Arg. of periapsis
121.6204°
True anomaly
238.43881°
Mean anomaly
248.4636°
Eccentric anomaly
243.40081°
Mean motion
3.32975 °/min
Orbital period
108.12 mins
BSTAR
0.00032969
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