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 64117U 26145.40180025 +.00000000 +00000-0 +47641-3 0 00005
2 64117 53.1607 30.0019 0001223 82.1975 277.9165 15.31719504 09
| Epoch (UTC): | 25 May 2026 09:38:35 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 30.0019° |
| argument of perigee: | 82.1975° |
| revolutions per day: | 15.31719504 |
| mean anomaly at epoch: | 277.9165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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