View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63252U 26145.25122992 +.00000000 +00000-0 +19693-3 0 00002
2 63252 97.6902 36.9198 0001347 337.1519 22.9641 14.94460136 05
| Epoch (UTC): | 25 May 2026 06:01:46 |
| Eccentricity: | 0.0001347 |
| inclination: | 97.6902° |
| perigee height: | 583 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 36.9198° |
| argument of perigee: | 337.1519° |
| revolutions per day: | 14.94460136 |
| mean anomaly at epoch: | 22.9641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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