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: 19 hours ago
TLE from 19 hours ago
0 EZIE-C
1 63249U 25052AR 26297.18566946 .00004074 00000-0 34894-3 0 9995
2 63249 97.6707 187.0781 0004718 117.4539 242.7164 14.98099413 87979Epoch: 2026-10-24T04:27Z
TLE epoch observation values (Epoch: 2026-10-24T04:27:21.841Z)
Latitude
0.00002°
Longitude
87.64161°
Altitude
577.327 km
Speed
7.571 km/s
True Right ascension
12h 28m 18s
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
18:31:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.054 km
Perigee altitude
566.498 km
Semi-major axis
6,947.913 km
Eccentricity
0.00047
Inclination
97.6707°
RAAN
187.0781°
Arg. of periapsis
117.4539°
True anomaly
242.66836°
Mean anomaly
242.7164°
Eccentric anomaly
242.69238°
Mean motion
3.74767 °/min
Orbital period
96.06 mins
BSTAR
0.00034894
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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 | 2026-10-25 05:04:48.158Z | 38.84° NE | 2026-10-25 05:07:48.158Z | 100.566° ESE | 31.881° | 2026-10-25 05:10:48.158Z | 157.343° SSE |
| 4 mins | 2026-10-25 06:40:48.158Z | 325.257° NNW | 2026-10-25 06:42:48.158Z | 289.185° WNW | 18.972° | 2026-10-25 06:44:48.158Z | 255.221° W |
| 4 mins | 2026-10-25 15:53:48.158Z | 90.22° ESE | 2026-10-25 15:54:48.158Z | 71.087° E | 19.416° | 2026-10-25 15:57:48.158Z | 22.442° NNE |
| 5 mins | 2026-10-25 17:27:48.158Z | 214.052° SW | 2026-10-25 17:29:48.158Z | 259.207° W | 31.254° | 2026-10-25 17:32:48.158Z | 320.543° NNW |
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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