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: 15 hours ago
TLE from 15 hours ago
0 EZIE-A
1 63247U 25052AP 26264.65712603 .00002667 00000-0 23119-3 0 9996
2 63247 97.6765 155.2500 0001246 189.1892 170.9308 14.97930134 83104Epoch: 2026-09-21T15:46Z
TLE epoch observation values (Epoch: 2026-09-21T15:46:15.688Z)
Latitude
-0.00003°
Longitude
-81.84917°
Altitude
577.201 km
Speed
7.572 km/s
True Right ascension
10h 21m 00s
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
23:48:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.165 km
Perigee altitude
569.434 km
Semi-major axis
6,948.437 km
Eccentricity
0.00012
Inclination
97.6765°
RAAN
155.25°
Arg. of periapsis
189.1892°
True anomaly
170.93305°
Mean anomaly
170.9308°
Eccentric anomaly
170.93193°
Mean motion
3.74725 °/min
Orbital period
96.07 mins
BSTAR
0.00023119
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-22 06:45:41.210Z | 333.672° NNW | 2026-09-22 06:48:41.210Z | 286.054° WNW | 16.892° | 2026-09-22 06:50:41.210Z | 255.331° W |
| 5 mins | 2026-09-22 15:58:41.210Z | 106.056° ESE | 2026-09-22 16:00:41.210Z | 68.257° E | 21.898° | 2026-09-22 16:03:41.210Z | 19.155° NNE |
| 5 mins | 2026-09-22 17:33:41.210Z | 219.819° SW | 2026-09-22 17:35:41.210Z | 263.227° W | 27.705° | 2026-09-22 17:38:41.210Z | 318.996° NNW |
| 6 mins | 2026-09-23 05:13:41.210Z | 37.119° NE | 2026-09-23 05:16:41.210Z | 114.59° SE | 38.122° | 2026-09-23 05:19:41.210Z | 166.172° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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