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 63386U 26145.50395803 +.00000000 +00000-0 +45092-3 0 00003
2 63386 53.1595 65.3316 0001854 90.7322 269.3893 15.34394064 00
| Epoch (UTC): | 25 May 2026 12:05:41 |
| Eccentricity: | 0.0001854 |
| inclination: | 53.1595° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 65.3316° |
| argument of perigee: | 90.7322° |
| revolutions per day: | 15.34394064 |
| mean anomaly at epoch: | 269.3893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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