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 57012U 26145.59374597 +.00000000 +00000-0 +45577-3 0 00006
2 57012 97.4912 257.7418 0007601 115.9188 244.2839 15.33768483 00
| Epoch (UTC): | 25 May 2026 14:14:59 |
| Eccentricity: | 0.0007601 |
| inclination: | 97.4912° |
| perigee height: | 459 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 257.7418° |
| argument of perigee: | 115.9188° |
| revolutions per day: | 15.33768483 |
| mean anomaly at epoch: | 244.2839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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