OBJECT E, 63214
Orbit data source: Space-Track
OBJECT E, 63214 is a 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). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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63214 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
Tel Aviv University (IL)Manufacturer
ISA/TAU
Mission
Operational Amateur Communications
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 OBJECT E
1 63214U 25052E 26129.64414968 .00013060 00000-0 41029-3 0 9991
2 63214 97.3940 25.9634 0001177 181.7304 178.3935 15.33125548 64204Epoch: 2026-05-09T15:27Z
TLE epoch observation values (Epoch: 2026-05-09T15:27:34.532Z)
Latitude
0.00004°
Longitude
-73.38912°
Altitude
470.408 km
Speed
7.63 km/s
True Right ascension
01h 43m 51s
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
14:20:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.247 km
Perigee altitude
462.636 km
Semi-major axis
6,841.579 km
Eccentricity
0.00012
Inclination
97.394°
RAAN
25.9634°
Arg. of periapsis
181.7304°
True anomaly
178.39388°
Mean anomaly
178.3935°
Eccentric anomaly
178.39369°
Mean motion
3.83538 °/min
Orbital period
93.86 mins
BSTAR
0.00041029
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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.OBJECT E 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 | 2026-05-10 06:08:27.275Z | 352.889° N | 2026-05-10 06:09:27.275Z | 315.83° NNW | 40.664° | 2026-05-10 06:12:27.275Z | 205.043° SW |
| 4 mins | 2026-05-10 16:40:27.275Z | 125.563° SE | 2026-05-10 16:42:27.275Z | 61.939° ENE | 29.819° | 2026-05-10 16:44:27.275Z | 13.727° NNE |
| 4 mins | 2026-05-11 05:38:27.275Z | 43.843° NE | 2026-05-11 05:39:27.275Z | 77.315° E | 34.381° | 2026-05-11 05:42:27.275Z | 169.653° S |
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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