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 57170U 26145.59968263 +.00000000 +00000-0 +35146-3 0 00001
2 57170 97.5132 207.1727 0009874 162.7560 197.4014 15.23751989 06
| Epoch (UTC): | 25 May 2026 14:23:32 |
| Eccentricity: | 0.0009874 |
| inclination: | 97.5132° |
| perigee height: | 488 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 207.1727° |
| argument of perigee: | 162.7560° |
| revolutions per day: | 15.23751989 |
| mean anomaly at epoch: | 197.4014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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