EZIE-B, 63250
Orbit data source: Space-Track
EZIE-B, 63250 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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63250 intel report (Beta)
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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 EZIE-B
1 63250U 25052AS 25312.18632390 .00010056 00000-0 93521-3 0 9990
2 63250 97.7097 203.0084 0002679 183.7889 176.3312 14.94524830 35621Epoch: 2025-11-08T04:28Z
TLE epoch observation values (Epoch: 2025-11-08T04:28:18.384Z)
Latitude
-0.00001°
Longitude
88.31225°
Altitude
588.757 km
Speed
7.565 km/s
True Right ascension
13h 32m 02s
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
04:26:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.725 km
Perigee altitude
578.997 km
Semi-major axis
6,958.998 km
Eccentricity
0.00027
Inclination
97.7097°
RAAN
203.0084°
Arg. of periapsis
183.7889°
True anomaly
176.33316°
Mean anomaly
176.3312°
Eccentric anomaly
176.33218°
Mean motion
3.73872 °/min
Orbital period
96.29 mins
BSTAR
0.00093521
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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-B 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 | 2025-11-08 15:52:28.519Z | 106.594° ESE | 2025-11-08 15:54:28.519Z | 75.726° E | 17.124° | 2025-11-08 15:57:28.519Z | 26.492° NE |
| 6 mins | 2025-11-08 17:27:28.519Z | 205.373° SW | 2025-11-08 17:30:28.519Z | 275.957° WNW | 29.064° | 2025-11-08 17:33:28.519Z | 326.612° NNW |
| 6 mins | 2025-11-09 05:09:28.519Z | 40.548° NE | 2025-11-09 05:12:28.519Z | 107.109° ESE | 28.205° | 2025-11-09 05:15:28.519Z | 159.512° S |
| 4 mins | 2025-11-09 06:45:28.519Z | 325.187° NNW | 2025-11-09 06:47:28.519Z | 289.59° WNW | 17.947° | 2025-11-09 06:49:28.519Z | 255.939° W |
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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