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 64292U 26145.31151477 +.00000000 +00000-0 -31913-3 0 00004
2 64292 70.0025 1.3524 0002903 273.9347 86.1481 14.98328406 06
| Epoch (UTC): | 25 May 2026 07:28:34 |
| Eccentricity: | 0.0002903 |
| inclination: | 70.0025° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3524° |
| argument of perigee: | 273.9347° |
| revolutions per day: | 14.98328406 |
| mean anomaly at epoch: | 86.1481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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