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 56797U 26145.38211343 +.00000000 +00000-0 +58308-4 0 00008
2 56797 69.9985 151.2556 0003946 267.3714 92.6993 14.98341862 03
| Epoch (UTC): | 25 May 2026 09:10:14 |
| Eccentricity: | 0.0003946 |
| inclination: | 69.9985° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 151.2556° |
| argument of perigee: | 267.3714° |
| revolutions per day: | 14.98341862 |
| mean anomaly at epoch: | 92.6993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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