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 56770U 26145.37415552 +.00000000 +00000-0 +42857-5 0 00009
2 56770 69.9984 171.1100 0003730 267.7787 92.2945 14.98331302 05
| Epoch (UTC): | 25 May 2026 08:58:47 |
| Eccentricity: | 0.0003730 |
| inclination: | 69.9984° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 171.1100° |
| argument of perigee: | 267.7787° |
| revolutions per day: | 14.98331302 |
| mean anomaly at epoch: | 92.2945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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