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 56816U 26145.36516612 +.00000000 +00000-0 -10032-3 0 00007
2 56816 69.9983 130.9322 0004068 265.0808 94.9887 14.98339854 08
| Epoch (UTC): | 25 May 2026 08:45:50 |
| Eccentricity: | 0.0004068 |
| inclination: | 69.9983° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 130.9322° |
| argument of perigee: | 265.0808° |
| revolutions per day: | 14.98339854 |
| mean anomaly at epoch: | 94.9887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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