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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Edit Public Description
Identifier
Orbit
Country
USRelated business
None
Manufacturer
Unknown
Mission
Operational Civil Science
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 EZIE-A
1 63247U 25052AP 25286.68493293 .00009010 00000-0 84995-3 0 9991
2 63247 97.7105 177.9189 0002772 333.0106 27.0969 14.93991106 31818Epoch: 2025-10-13T16:26Z
TLE epoch observation values (Epoch: 2025-10-13T16:26:18.205Z)
Latitude
-0.00006°
Longitude
-91.14112°
Altitude
586.833 km
Speed
7.568 km/s
True Right ascension
11h 51m 40s
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
11:59:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.449 km
Perigee altitude
580.59 km
Semi-major axis
6,960.657 km
Eccentricity
0.00028
Inclination
97.7105°
RAAN
177.9189°
Arg. of periapsis
333.0106°
True anomaly
27.11137°
Mean anomaly
27.0969°
Eccentric anomaly
27.10414°
Mean motion
3.73739 °/min
Orbital period
96.32 mins
BSTAR
0.00084995
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-15 05:58:07.982Z | 4.04° NNE | 2025-10-15 06:02:07.982Z | 255.692° W | 40.388° | 2025-10-15 06:05:07.982Z | 206.767° SW |
| 6 mins | 2025-10-15 16:48:07.982Z | 158.902° S | 2025-10-15 16:50:07.982Z | 127.055° SE | 43.268° | 2025-10-15 16:54:07.982Z | 351.204° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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