COSMOS 1579 FUEL CORE, 15330

Orbit data source: Space-Track

COSMOS 1579 FUEL CORE, 15330 is space debris in LEO originally from a launch on Fri, 29 Jun 1984 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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.

Loading next visibility...
Identifier
15330, 1984-069D
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
Kometa
Mission
Spacecraft
Bus & Motor
US-A REACTOR CORE, Unknown motor
Mass
Wet unknown, 53 kg dry
Launch date (UTC)
1984-06-29 (42 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 COSMOS 1579 FUEL CORE
1 15330U 84069D   26258.65975906 -.00000076  00000-0  11258-4 0  9994
2 15330  65.0558 311.6331 0050075 284.3712 158.1729 13.89920706144552
Epoch: 2026-09-15T15:50Z
TLE epoch observation values (Epoch: 2026-09-15T15:50:03.182Z)
Latitude
64.20495°
Longitude
152.70627°
Altitude
972.992 km
Speed
7.354 km/s
True Right ascension
01h 39m 22s
True Declination
64° 04' 26"
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
14:02:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
964.091 km
Perigee altitude
890.925 km
Semi-major axis
7,305.645 km
Eccentricity
0.00501
Inclination
65.0558°
RAAN
311.6331°
Arg. of periapsis
284.3712°
True anomaly
158.38502°
Mean anomaly
158.1729°
Eccentric anomaly
158.27908°
Mean motion
3.4758 °/min
Orbital period
103.57 mins
BSTAR
0.000011258
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|