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 57214U 26145.35669814 +.00000000 +00000-0 +00000-0 0 00002
2 57214 0.0153 316.8107 0000212 137.1766 270.8942 1.00270506 05
| Epoch (UTC): | 25 May 2026 08:33:38 |
| Eccentricity: | 0.0000212 |
| inclination: | 0.0153° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 316.8107° |
| argument of perigee: | 137.1766° |
| revolutions per day: | 1.00270506 |
| mean anomaly at epoch: | 270.8942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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