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 57218U 26145.49763806 +.00000000 +00000-0 +15186-4 0 00002
2 57218 43.0002 316.8387 0001120 260.6087 99.4638 15.27575177 09
| Epoch (UTC): | 25 May 2026 11:56:35 |
| Eccentricity: | 0.0001120 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.8387° |
| argument of perigee: | 260.6087° |
| revolutions per day: | 15.27575177 |
| mean anomaly at epoch: | 99.4638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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