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 57074U 26145.40513713 +.00000000 +00000-0 +65160-4 0 00000
2 57074 43.0053 40.9360 0000911 237.1049 122.9715 15.27587829 00
| Epoch (UTC): | 25 May 2026 09:43:23 |
| Eccentricity: | 0.0000911 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.9360° |
| argument of perigee: | 237.1049° |
| revolutions per day: | 15.27587829 |
| mean anomaly at epoch: | 122.9715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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