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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 (1 year 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: 16 hours ago

TLE from 16 hours ago
0 EZIE-A
1 63247U 25052AP  26083.95673935  .00004870  00000-0  43365-3 0  9995
2 63247  97.6981 337.4705 0004127 111.4290 248.7372 14.96495216 56062
Epoch: 2026-03-24T22:57Z
TLE epoch observation values (Epoch: 2026-03-24T22:57:42.279Z)
Latitude
-0.00005°
Longitude
170.61739°
Altitude
581.828 km
Speed
7.569 km/s
True Right ascension
22h 29m 52s
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
20:30:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.615 km
Perigee altitude
571.876 km
Semi-major axis
6,952.882 km
Eccentricity
0.00041
Inclination
97.6981°
RAAN
337.4705°
Arg. of periapsis
111.429°
True anomaly
248.69314°
Mean anomaly
248.7372°
Eccentric anomaly
248.71517°
Mean motion
3.74366 °/min
Orbital period
96.16 mins
BSTAR
0.00043365
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Documentation

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