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 57201U 26145.56438735 +.00000000 +00000-0 +52341-3 0 00005
2 57201 97.5090 215.3287 0008157 146.7234 213.4525 15.37159871 02
| Epoch (UTC): | 25 May 2026 13:32:43 |
| Eccentricity: | 0.0008157 |
| inclination: | 97.5090° |
| perigee height: | 449 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 215.3287° |
| argument of perigee: | 146.7234° |
| revolutions per day: | 15.37159871 |
| mean anomaly at epoch: | 213.4525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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