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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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: 7 hours ago
TLE from 7 hours ago
0 EZIE-B
1 63250U 25052AS 26121.18150222 .00007832 00000-0 68670-3 0 9993
2 63250 97.6960 14.1585 0003784 22.5397 337.5990 14.96911425 61633Epoch: 2026-05-01T04:21Z
TLE epoch observation values (Epoch: 2026-05-01T04:21:21.791Z)
Latitude
-0.00008°
Longitude
89.70027°
Altitude
577.063 km
Speed
7.573 km/s
True Right ascension
00h 56m 38s
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
19:21:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.086 km
Perigee altitude
570.825 km
Semi-major axis
6,951.592 km
Eccentricity
0.00038
Inclination
97.696°
RAAN
14.1585°
Arg. of periapsis
22.5397°
True anomaly
337.58247°
Mean anomaly
337.599°
Eccentric anomaly
337.59073°
Mean motion
3.7447 °/min
Orbital period
96.14 mins
BSTAR
0.0006867
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-01 15:45:06.593Z | 96.117° ESE | 2026-05-01 15:47:06.593Z | 64.252° ENE | 14.728° | 2026-05-01 15:49:06.593Z | 33.29° NE |
| 6 mins | 2026-05-01 17:19:06.593Z | 196.747° SSW | 2026-05-01 17:22:06.593Z | 269.634° W | 33.157° | 2026-05-01 17:25:06.593Z | 329.02° NNW |
| 5 mins | 2026-05-02 05:01:06.593Z | 56.823° ENE | 2026-05-02 05:03:06.593Z | 101.86° ESE | 24.059° | 2026-05-02 05:06:06.593Z | 152.526° SSE |
| 5 mins | 2026-05-02 06:36:06.593Z | 328.143° NNW | 2026-05-02 06:38:06.593Z | 288.746° WNW | 21.02° | 2026-05-02 06:41:06.593Z | 240.205° WSW |
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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