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 66195U 26145.55936655 +.00000000 +00000-0 +39826-3 0 00003
2 66195 53.1594 248.1440 0001116 89.7524 270.3604 15.30201548 04
| Epoch (UTC): | 25 May 2026 13:25:29 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.1440° |
| argument of perigee: | 89.7524° |
| revolutions per day: | 15.30201548 |
| mean anomaly at epoch: | 270.3604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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