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 57764U 26145.43423209 +.00000000 +00000-0 +73972-4 0 00009
2 57764 81.0014 28.8359 0007401 64.6007 295.5915 13.85726877 05
| Epoch (UTC): | 25 May 2026 10:25:17 |
| Eccentricity: | 0.0007401 |
| inclination: | 81.0014° |
| perigee height: | 938 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 28.8359° |
| argument of perigee: | 64.6007° |
| revolutions per day: | 13.85726877 |
| mean anomaly at epoch: | 295.5915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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