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 56785U 26145.37376633 +.00000000 +00000-0 +12704-4 0 00008
2 56785 69.9986 151.2338 0003910 266.2517 93.8195 14.98331378 07
| Epoch (UTC): | 25 May 2026 08:58:13 |
| Eccentricity: | 0.0003910 |
| inclination: | 69.9986° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 151.2338° |
| argument of perigee: | 266.2517° |
| revolutions per day: | 14.98331378 |
| mean anomaly at epoch: | 93.8195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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