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 55766U 26145.40157891 +.00000000 +00000-0 -29313-4 0 00008
2 55766 70.0002 31.0480 0002774 268.4824 91.6017 14.98329848 00
| Epoch (UTC): | 25 May 2026 09:38:16 |
| Eccentricity: | 0.0002774 |
| inclination: | 70.0002° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.0480° |
| argument of perigee: | 268.4824° |
| revolutions per day: | 14.98329848 |
| mean anomaly at epoch: | 91.6017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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