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 64370U 26145.57420941 +.00000000 +00000-0 +16515-2 0 00003
2 64370 43.0012 341.1643 0002043 267.7771 92.2862 15.70899840 00
| Epoch (UTC): | 25 May 2026 13:46:51 |
| Eccentricity: | 0.0002043 |
| inclination: | 43.0012° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 341.1643° |
| argument of perigee: | 267.7771° |
| revolutions per day: | 15.70899840 |
| mean anomaly at epoch: | 92.2862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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