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 57180U 26145.59926308 +.00000000 +00000-0 +37925-3 0 00003
2 57180 97.5097 208.8869 0012247 172.0484 188.0952 15.27307588 02
| Epoch (UTC): | 25 May 2026 14:22:56 |
| Eccentricity: | 0.0012247 |
| inclination: | 97.5097° |
| perigee height: | 475 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 208.8869° |
| argument of perigee: | 172.0484° |
| revolutions per day: | 15.27307588 |
| mean anomaly at epoch: | 188.0952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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