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 56777U 26145.45304997 +.00000000 +00000-0 -63046-4 0 00008
2 56777 69.9994 151.1105 0003353 265.3746 94.7031 14.98325841 00
| Epoch (UTC): | 25 May 2026 10:52:23 |
| Eccentricity: | 0.0003353 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 151.1105° |
| argument of perigee: | 265.3746° |
| revolutions per day: | 14.98325841 |
| mean anomaly at epoch: | 94.7031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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