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 66381U 26145.46922693 +.00000000 +00000-0 +59834-3 0 00008
2 66381 53.1597 220.7576 0001672 88.0180 272.1012 15.30185573 09
| Epoch (UTC): | 25 May 2026 11:15:41 |
| Eccentricity: | 0.0001672 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 220.7576° |
| argument of perigee: | 88.0180° |
| revolutions per day: | 15.30185573 |
| mean anomaly at epoch: | 272.1012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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