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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
7 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 (7 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, 30.5 m
Radar Cross Section
20.330 m²

Expand to show TLE details & history

TLE from 7 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
Definitive object data (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 TLE epoch
Visualization TLE readout
Latitude
31.42557°
Longitude
95.04476°
Altitude
173.686 km
Speed
7.805 km/s
Apparent Right ascension
00h 42m 14s
Apparent Declination
-3° 43' 11"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
13:20:22
Azimuth
15.86° NNE
Elevation
-52.79°
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
BSTAR
Unknown
Orbital period
87.95 mins
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Other satellites on launch #182 in the year 2024 (2024-10-14 UTC)

EUROPA CLIPPER Visibility forecast

Observer location: undefined°, undefined°

EUROPA CLIPPER is not visible in the next 10 days
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