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 64314U 26145.02363845 +.00000000 +00000-0 +48986-3 0 00008
2 64314 70.0013 1.9529 0002550 266.0942 93.9925 14.98336263 00
| Epoch (UTC): | 25 May 2026 00:34:02 |
| Eccentricity: | 0.0002550 |
| inclination: | 70.0013° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.9529° |
| argument of perigee: | 266.0942° |
| revolutions per day: | 14.98336263 |
| mean anomaly at epoch: | 93.9925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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