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 57037U 26145.58787442 +.00000000 +00000-0 +19030-3 0 00004
2 57037 97.4845 251.2248 0006717 169.1213 191.0167 15.18020774 09
| Epoch (UTC): | 25 May 2026 14:06:32 |
| Eccentricity: | 0.0006717 |
| inclination: | 97.4845° |
| perigee height: | 507 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 251.2248° |
| argument of perigee: | 169.1213° |
| revolutions per day: | 15.18020774 |
| mean anomaly at epoch: | 191.0167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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