CICERO 6, 42793 (Decayed)

Orbit data source: Space-Track

CICERO 6, 42793 was a payload satellite owned by GeoOptics (US) in LEO that was launched on Fri, 23 Jun 2017 UTC via a PSLV-XL launch vehicle from the Sirharikota (SRI). 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

CICERO 6 details

Identifier	42793, 2017-036AE
Orbit	Decayed
Last TLE update	7 months ago
Origin	GeoOptics (US)
Manufacturer	Tyvak NSS
Mission	Decayed Commercial Weather
Bus & Motor	CUBESAT 6U, Unknown motor
Mass	8 kg wet, 8 kg dry
Launch date (UTC)	2017-06-23 (8 years ago)
Launch vehicle	PSLV-XL
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, 0.6 m
Radar Cross Section	0.079 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 7 months ago

0 CICERO 6
1 42793U 17036AE  24163.54141734  .14136259  24115-5  22659-3 0  9993
2 42793  97.0194 202.5662 0010261 237.3230 122.7085 16.47770263388951

Epoch: 2024-06-11T12:59Z

Definitive object data (Epoch: 2024-06-11T12:59:38.458Z)

Latitude	-0.00005°
Longitude	107.29481°
Altitude	152.109 km
Speed	7.813 km/s
True Right ascension	13h 30m 15s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow 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	148.685 km
Perigee altitude	135.304 km
Semi-major axis	6,520.132 km
Eccentricity	0.0010261
Inclination	97.0194°
RAAN	202.5662°
Arg. of periapsis	237.323°
True anomaly	122.80737°
Mean anomaly	122.7085°
Eccentric anomaly	122.75794°
Mean motion	4.12248 °/min
BSTAR	0.00022659
Orbital period	87.33 mins