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 64774U 26145.53776294 +.00000000 +00000-0 +60703-4 0 00002
2 64774 53.1623 246.0698 0000383 177.7007 182.3996 15.30199249 09
| Epoch (UTC): | 25 May 2026 12:54:22 |
| Eccentricity: | 0.0000383 |
| inclination: | 53.1623° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 246.0698° |
| argument of perigee: | 177.7007° |
| revolutions per day: | 15.30199249 |
| mean anomaly at epoch: | 182.3996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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