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 57110U 26145.45078118 +.00000000 +00000-0 +38765-4 0 00002
2 57110 43.0017 207.9110 0001576 272.0213 88.0457 15.26743121 01
| Epoch (UTC): | 25 May 2026 10:49:07 |
| Eccentricity: | 0.0001576 |
| inclination: | 43.0017° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 207.9110° |
| argument of perigee: | 272.0213° |
| revolutions per day: | 15.26743121 |
| mean anomaly at epoch: | 88.0457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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