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 64569U 26145.61825443 +.00000000 +00000-0 +15843-3 0 00008
2 64569 97.7728 260.1564 0003118 81.6686 278.4888 14.93556956 02
| Epoch (UTC): | 25 May 2026 14:50:17 |
| Eccentricity: | 0.0003118 |
| inclination: | 97.7728° |
| perigee height: | 585 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 260.1564° |
| argument of perigee: | 81.6686° |
| revolutions per day: | 14.93556956 |
| mean anomaly at epoch: | 278.4888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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