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 61569U 26145.60317465 +.00000000 +00000-0 +15688-3 0 00001
2 61569 88.9808 63.9576 0004326 300.7041 59.3686 13.55631310 01
| Epoch (UTC): | 25 May 2026 14:28:34 |
| Eccentricity: | 0.0004326 |
| inclination: | 88.9808° |
| perigee height: | 1048 km |
| apogee height: | 1055 km |
| right ascension of ascending node: | 63.9576° |
| argument of perigee: | 300.7041° |
| revolutions per day: | 13.55631310 |
| mean anomaly at epoch: | 59.3686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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