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 57066U 26145.39022116 +.00000000 +00000-0 +34224-4 0 00008
2 57066 43.0054 37.4114 0000957 257.6063 102.4682 15.27579174 03
| Epoch (UTC): | 25 May 2026 09:21:55 |
| Eccentricity: | 0.0000957 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.4114° |
| argument of perigee: | 257.6063° |
| revolutions per day: | 15.27579174 |
| mean anomaly at epoch: | 102.4682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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