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 62066U 26145.47239314 +.00000000 +00000-0 +12563-2 0 00003
2 62066 53.1581 52.7078 0001562 90.7795 269.3402 15.69755541 09
| Epoch (UTC): | 25 May 2026 11:20:14 |
| Eccentricity: | 0.0001562 |
| inclination: | 53.1581° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 52.7078° |
| argument of perigee: | 90.7795° |
| revolutions per day: | 15.69755541 |
| mean anomaly at epoch: | 269.3402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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