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 66101U 26145.31617801 +.00000000 +00000-0 +63495-3 0 00002
2 66101 53.1576 108.1492 0001235 101.4537 258.6603 15.30211029 04
| Epoch (UTC): | 25 May 2026 07:35:17 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.1492° |
| argument of perigee: | 101.4537° |
| revolutions per day: | 15.30211029 |
| mean anomaly at epoch: | 258.6603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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