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 57091U 26145.65483951 +.00000000 +00000-0 +67026-4 0 00009
2 57091 43.0060 21.2499 0001346 261.4147 98.6552 15.27577390 04
| Epoch (UTC): | 25 May 2026 15:42:58 |
| Eccentricity: | 0.0001346 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.2499° |
| argument of perigee: | 261.4147° |
| revolutions per day: | 15.27577390 |
| mean anomaly at epoch: | 98.6552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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