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 57349U 26145.42557904 +.00000000 +00000-0 +63251-5 0 00007
2 57349 43.0013 175.5020 0001547 266.3852 93.6823 15.27575708 08
| Epoch (UTC): | 25 May 2026 10:12:50 |
| Eccentricity: | 0.0001547 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.5020° |
| argument of perigee: | 266.3852° |
| revolutions per day: | 15.27575708 |
| mean anomaly at epoch: | 93.6823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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