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 26067.51855910 +.00000000 +00000-0 +51076-3 0 00002
2 57172 97.5175 126.6294 0014603 109.7259 250.5553 15.19577080 03
| Epoch (UTC): | 08 March 2026 12:26:43 |
| Eccentricity: | 0.0014603 |
| inclination: | 97.5175° |
| perigee height: | 497 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 126.6294° |
| argument of perigee: | 109.7259° |
| revolutions per day: | 15.19577080 |
| mean anomaly at epoch: | 250.5553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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