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 64592U 26145.58102584 +.00000000 +00000-0 +14282-3 0 00000
2 64592 97.7730 260.5162 0004149 74.1333 286.0343 14.93719203 07
| Epoch (UTC): | 25 May 2026 13:56:40 |
| Eccentricity: | 0.0004149 |
| inclination: | 97.7730° |
| perigee height: | 583 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 260.5162° |
| argument of perigee: | 74.1333° |
| revolutions per day: | 14.93719203 |
| mean anomaly at epoch: | 286.0343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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