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 57174U 26145.58251647 +.00000000 +00000-0 +17583-3 0 00000
2 57174 97.5070 199.0023 0012271 220.2119 139.8205 15.13745183 04
| Epoch (UTC): | 25 May 2026 13:58:49 |
| Eccentricity: | 0.0012271 |
| inclination: | 97.5070° |
| perigee height: | 516 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 199.0023° |
| argument of perigee: | 220.2119° |
| revolutions per day: | 15.13745183 |
| mean anomaly at epoch: | 139.8205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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