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EZIE-A, 63247

Orbit data source: Space-Track

EZIE-A, 63247 is an American payload satellite in SSO that was launched on Sat, 15 Mar 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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.

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Identifier
63247, 2025-052AP
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
APL
Mission
Operational Civil Science
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2025-03-15 (10 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 EZIE-A
1 63247U 25052AP  26027.64275288  .00009066  00000-0  81840-3 0  9990
2 63247  97.7061 282.0648 0002429 343.4306  16.6835 14.95727472 47642
Epoch: 2026-01-27T15:25Z
TLE epoch observation values (Epoch: 2026-01-27T15:25:33.848Z)
Latitude
-0.00008°
Longitude
-76.24744°
Altitude
581.545 km
Speed
7.571 km/s
True Right ascension
18h 48m 15s
True Declination
0° 00' 00"
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
22:31:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.816 km
Perigee altitude
575.437 km
Semi-major axis
6,955.264 km
Eccentricity
0.00024
Inclination
97.7061°
RAAN
282.0648°
Arg. of periapsis
343.4306°
True anomaly
16.69149°
Mean anomaly
16.6835°
Eccentric anomaly
16.6875°
Mean motion
3.74173 °/min
Orbital period
96.21 mins
BSTAR
0.0008184
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