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 66103U 26145.30667980 +.00000000 +00000-0 +82190-3 0 00009
2 66103 53.1581 108.0891 0001054 91.1967 268.9155 15.30195012 04
| Epoch (UTC): | 25 May 2026 07:21:37 |
| Eccentricity: | 0.0001054 |
| inclination: | 53.1581° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.0891° |
| argument of perigee: | 91.1967° |
| revolutions per day: | 15.30195012 |
| mean anomaly at epoch: | 268.9155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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