EZIE-C, 63249
Orbit data source: Space-Track
EZIE-C, 63249 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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63249 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: 12 hours ago
TLE from 12 hours ago
0 EZIE-C
1 63249U 25052AR 26260.51333431 .00003916 00000-0 33768-3 0 9996
2 63249 97.6731 151.0355 0000948 260.2563 99.8553 14.97868794 82488Epoch: 2026-09-17T12:19Z
TLE epoch observation values (Epoch: 2026-09-17T12:19:12.084Z)
Latitude
0.00005°
Longitude
-30.21435°
Altitude
576.648 km
Speed
7.572 km/s
True Right ascension
10h 04m 08s
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
17:19:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.148 km
Perigee altitude
569.831 km
Semi-major axis
6,948.626 km
Eccentricity
0.00009
Inclination
97.6731°
RAAN
151.0355°
Arg. of periapsis
260.2563°
True anomaly
99.866°
Mean anomaly
99.8553°
Eccentric anomaly
99.86065°
Mean motion
3.7471 °/min
Orbital period
96.07 mins
BSTAR
0.00033768
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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-C 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 04:56:08.669Z | 45.419° ENE | 2026-09-18 04:59:08.669Z | 102.825° ESE | 25.068° | 2026-09-18 05:02:08.669Z | 151.484° SSE |
| 5 mins | 2026-09-18 06:32:08.669Z | 327.412° NNW | 2026-09-18 06:34:08.669Z | 286.027° WNW | 23.686° | 2026-09-18 06:37:08.669Z | 237.887° WSW |
| 5 mins | 2026-09-18 17:19:08.669Z | 205.837° SW | 2026-09-18 17:21:08.669Z | 259.664° W | 40.19° | 2026-09-18 17:24:08.669Z | 326.635° 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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