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 65765U 26145.54998109 +.00000000 +00000-0 -21386-1 0 00007
2 65765 51.8863 41.7742 0008226 199.5213 160.5445 15.01624560 00
| Epoch (UTC): | 25 May 2026 13:11:58 |
| Eccentricity: | 0.0008226 |
| inclination: | 51.8863° |
| perigee height: | 556 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 41.7742° |
| argument of perigee: | 199.5213° |
| revolutions per day: | 15.01624560 |
| mean anomaly at epoch: | 160.5445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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