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 64107U 26144.96871887 +.00000000 +00000-0 +57657-3 0 00005
2 64107 53.1599 32.2785 0001164 81.0167 279.0966 15.31708230 03
| Epoch (UTC): | 24 May 2026 23:14:57 |
| Eccentricity: | 0.0001164 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 32.2785° |
| argument of perigee: | 81.0167° |
| revolutions per day: | 15.31708230 |
| mean anomaly at epoch: | 279.0966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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