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EUROPA CLIPPER, 61507

Orbit data source: Space-Track

EUROPA CLIPPER, 61507 is a payload satellite owned by JPL (US) in LEO that was launched on Mon, 14 Oct 2024 UTC via an FALCON HEAVY launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft 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
Identifier
61507, 2024-182A
Orbit
LEO
Last TLE update
10 months ago
Origin
Manufacturer
JPL
Mission
Operational Civil Planetary
Bus & Motor
EUROPA, AOCS
Mass
5,700 kg wet, 3,241 kg dry
Launch date (UTC)
2024-10-14 (10 months ago)
Launch vehicle
FALCON HEAVY
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 15.3 m
Radar Cross Section
20.330 m²

Expand to show TLE details & history

TLE from 10 months ago
0 EUROPA CLIPPER
1 61507U 24182A   24288.67632810  .00000840 -26562-5  00000-0 0  9992
2 61507  31.9400  67.0176 0018900  60.7600  70.5300 16.38814738    06
Epoch: 2024-10-14T16:13Z
TLE epoch observation values (Epoch: 2024-10-14T16:13:54.747Z)
Latitude
23.45054°
Longitude
-63.93444°
Altitude
163.258 km
Speed
7.816 km/s
True Right ascension
13h 32m 58s
True Declination
23° 18' 50"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-27.58538°
Longitude
-147.74071°
Altitude
186.985 km
Speed
7.788 km/s
Apparent Right ascension
04h 24m 10s
Apparent Declination
-74° 12' 13"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
09:14:32
Azimuth
198.195° SSW
Elevation
-33.709°
Doppler factor
1
Orbital elements
Apogee altitude
185.247 km
Perigee altitude
160.485 km
Semi-major axis
6,551.003 km
Eccentricity
0.00189
Inclination
31.94°
RAAN
67.0176°
Arg. of periapsis
60.76°
True anomaly
70.73435°
Mean anomaly
70.53°
Eccentric anomaly
70.63216°
Mean motion
4.09337 °/min
Orbital period
87.95 mins
BSTAR
0
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