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 66026U 26145.50003470 +.00000000 +00000-0 -28915-3 0 00009
2 66026 53.1590 107.2909 0000945 90.5847 257.6519 15.34412861 04
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0000945 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 107.2909° |
| argument of perigee: | 90.5847° |
| revolutions per day: | 15.34412861 |
| mean anomaly at epoch: | 257.6519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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