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 66099U 26145.33400495 +.00000000 +00000-0 +68678-3 0 00007
2 66099 53.1574 107.5497 0001292 76.5500 283.5645 15.30216227 09
| Epoch (UTC): | 25 May 2026 08:00:58 |
| Eccentricity: | 0.0001292 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 107.5497° |
| argument of perigee: | 76.5500° |
| revolutions per day: | 15.30216227 |
| mean anomaly at epoch: | 283.5645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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