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 65318U 26145.45409929 +.00000000 +00000-0 +55039-3 0 00001
2 65318 97.7385 220.9374 0002913 331.9986 28.1077 14.94440984 07
| Epoch (UTC): | 25 May 2026 10:53:54 |
| Eccentricity: | 0.0002913 |
| inclination: | 97.7385° |
| perigee height: | 582 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 220.9374° |
| argument of perigee: | 331.9986° |
| revolutions per day: | 14.94440984 |
| mean anomaly at epoch: | 28.1077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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