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 55659U 26145.48017073 +.00000000 +00000-0 -30535-4 0 00002
2 55659 69.9989 330.9746 0002667 264.8897 95.1957 14.98329675 09
| Epoch (UTC): | 25 May 2026 11:31:26 |
| Eccentricity: | 0.0002667 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.9746° |
| argument of perigee: | 264.8897° |
| revolutions per day: | 14.98329675 |
| mean anomaly at epoch: | 95.1957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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