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 66955U 26145.38669104 +.00000000 +00000-0 +38878-4 0 00007
2 66955 86.4871 289.9848 0001590 112.9659 247.1643 13.24410211 09
| Epoch (UTC): | 25 May 2026 09:16:50 |
| Eccentricity: | 0.0001590 |
| inclination: | 86.4871° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 289.9848° |
| argument of perigee: | 112.9659° |
| revolutions per day: | 13.24410211 |
| mean anomaly at epoch: | 247.1643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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