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 57172U 26145.58953995 +.00000000 +00000-0 +26149-3 0 00001
2 57172 97.5065 204.3768 0012634 191.1680 168.9276 15.20511601 09
| Epoch (UTC): | 25 May 2026 14:08:56 |
| Eccentricity: | 0.0012634 |
| inclination: | 97.5065° |
| perigee height: | 496 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 204.3768° |
| argument of perigee: | 191.1680° |
| revolutions per day: | 15.20511601 |
| mean anomaly at epoch: | 168.9276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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