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 66420U 26145.31746422 +.00000000 +00000-0 +89276-4 0 00004
2 66420 50.0041 17.3283 0001006 55.5344 304.5623 13.29322860 06
| Epoch (UTC): | 25 May 2026 07:37:08 |
| Eccentricity: | 0.0001006 |
| inclination: | 50.0041° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 17.3283° |
| argument of perigee: | 55.5344° |
| revolutions per day: | 13.29322860 |
| mean anomaly at epoch: | 304.5623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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