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 65697U 26145.57855368 +.00000000 +00000-0 +69544-3 0 00002
2 65697 53.1588 347.2496 0001113 308.2184 51.8719 15.34409056 00
| Epoch (UTC): | 25 May 2026 13:53:07 |
| Eccentricity: | 0.0001113 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 347.2496° |
| argument of perigee: | 308.2184° |
| revolutions per day: | 15.34409056 |
| mean anomaly at epoch: | 51.8719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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