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 64017U 26145.36708212 +.00000000 +00000-0 +63806-3 0 00004
2 64017 42.9971 284.7859 0000733 281.7101 78.3669 15.27595756 09
| Epoch (UTC): | 25 May 2026 08:48:35 |
| Eccentricity: | 0.0000733 |
| inclination: | 42.9971° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 284.7859° |
| argument of perigee: | 281.7101° |
| revolutions per day: | 15.27595756 |
| mean anomaly at epoch: | 78.3669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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