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 65094U 26144.97286735 +.00000000 +00000-0 +10520-2 0 00001
2 65094 53.1590 29.8774 0001452 311.9875 48.1007 15.42163408 06
| Epoch (UTC): | 24 May 2026 23:20:55 |
| Eccentricity: | 0.0001452 |
| inclination: | 53.1590° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 29.8774° |
| argument of perigee: | 311.9875° |
| revolutions per day: | 15.42163408 |
| mean anomaly at epoch: | 48.1007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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