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 65078U 26145.09198583 +.00000000 +00000-0 +92690-3 0 00009
2 65078 53.1597 29.2533 0001043 85.9344 274.1776 15.30202982 09
| Epoch (UTC): | 25 May 2026 02:12:27 |
| Eccentricity: | 0.0001043 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.2533° |
| argument of perigee: | 85.9344° |
| revolutions per day: | 15.30202982 |
| mean anomaly at epoch: | 274.1776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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