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 57188U 26145.56086565 +.00000000 +00000-0 +32031-3 0 00003
2 57188 97.5081 209.0243 0009630 162.8261 197.3305 15.26260704 06
| Epoch (UTC): | 25 May 2026 13:27:38 |
| Eccentricity: | 0.0009630 |
| inclination: | 97.5081° |
| perigee height: | 480 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 209.0243° |
| argument of perigee: | 162.8261° |
| revolutions per day: | 15.26260704 |
| mean anomaly at epoch: | 197.3305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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