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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63247 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Operational Civil Science
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 EZIE-A
1 63247U 25052AP 26259.51344750 .00003600 00000-0 31053-3 0 9993
2 63247 97.6755 150.1920 0001004 223.9564 136.1579 14.97902328 82330Epoch: 2026-09-16T12:19Z
TLE epoch observation values (Epoch: 2026-09-16T12:19:21.864Z)
Latitude
-0.00001°
Longitude
-30.11305°
Altitude
576.935 km
Speed
7.572 km/s
True Right ascension
10h 00m 46s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:01:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.083 km
Perigee altitude
569.688 km
Semi-major axis
6,948.523 km
Eccentricity
0.0001
Inclination
97.6755°
RAAN
150.192°
Arg. of periapsis
223.9564°
True anomaly
136.16587°
Mean anomaly
136.1579°
Eccentric anomaly
136.16188°
Mean motion
3.74718 °/min
Orbital period
96.07 mins
BSTAR
0.00031053
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Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EZIE-A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-18 04:59:18.692Z | 45.706° ENE | 2026-09-18 05:02:18.692Z | 107.05° ESE | 26.366° | 2026-09-18 05:05:18.692Z | 154.446° SSE |
| 4 mins | 2026-09-18 06:35:18.692Z | 323.947° NNW | 2026-09-18 06:37:18.692Z | 282.914° WNW | 22.121° | 2026-09-18 06:39:18.692Z | 248.167° W |
| 5 mins | 2026-09-18 17:22:18.692Z | 210.776° SW | 2026-09-18 17:24:18.692Z | 266.043° W | 37.501° | 2026-09-18 17:27:18.692Z | 326.348° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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