ASAP-S, 41461 (Decayed)

Orbit data source: Space-Track

ASAP-S, 41461 was a payload satellite owned by CNES (FR) in LEO that was launched on Mon, 25 Apr 2016 UTC launched from the French Guiana (FRGUI). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days

ASAP-S details

Identifier	41461, 2016-025F
Orbit	Decayed
Last TLE update	5 months ago
Origin	CNES (FR)
Manufacturer	Airbus Barajas
Mission	Decayed spacecraft
Bus & Motor	DISPENSER, Unknown motor
Mass	400 kg wet, 400 kg dry
Launch date (UTC)	2016-04-25 (9 years ago)
Launch vehicle	Unknown
Launch site	French Guiana (FRGUI)
Object type	Payload Rocket body Debris
Shape & HBR	Irr, 1.2 m
Radar Cross Section	1.920 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 5 months ago

0 ASAP-S
1 41461U 16025F   24222.51379594  .21966838  34272-5  59042-3 0  9994
2 41461  98.1082 124.4953 0004177 195.9430 250.6342 16.45604282457370

Epoch: 2024-08-09T12:19Z

Definitive object data (Epoch: 2024-08-09T12:19:51.969Z)

Latitude	81.23409°
Longitude	-85.6806°
Altitude	165.28 km
Speed	7.813 km/s
True Right ascension	03h 51m 05s
True Declination	81° 10' 39"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	150.496 km
Perigee altitude	145.045 km
Semi-major axis	6,525.907 km
Eccentricity	0.0004177
Inclination	98.1082°
RAAN	124.4953°
Arg. of periapsis	195.943°
True anomaly	250.58905°
Mean anomaly	250.6342°
Eccentric anomaly	250.61162°
Mean motion	4.11701 °/min
BSTAR	0.00059042
Orbital period	87.44 mins