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 56796U 26145.43635216 +.00000000 +00000-0 +44695-4 0 00006
2 56796 69.9985 151.0507 0003638 266.1678 93.9065 14.98332518 02
| Epoch (UTC): | 25 May 2026 10:28:20 |
| Eccentricity: | 0.0003638 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 151.0507° |
| argument of perigee: | 266.1678° |
| revolutions per day: | 14.98332518 |
| mean anomaly at epoch: | 93.9065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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