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 66100U 26145.58335647 +.00000000 +00000-0 -43392-3 0 00000
2 66100 53.1595 106.8676 0001013 77.7748 336.2045 15.34394488 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 106.8676° |
| argument of perigee: | 77.7748° |
| revolutions per day: | 15.34394488 |
| mean anomaly at epoch: | 336.2045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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