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 65692U 26145.30205012 +.00000000 +00000-0 +54706-3 0 00007
2 65692 53.1609 349.7859 0001013 79.7703 280.3412 15.30208317 07
| Epoch (UTC): | 25 May 2026 07:14:57 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.7859° |
| argument of perigee: | 79.7703° |
| revolutions per day: | 15.30208317 |
| mean anomaly at epoch: | 280.3412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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