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 57603U 26145.35190278 +.00000000 +00000-0 +11910-2 0 00001
2 57603 43.0009 21.1588 0005332 232.7440 127.2919 15.09710925 09
| Epoch (UTC): | 25 May 2026 08:26:44 |
| Eccentricity: | 0.0005332 |
| inclination: | 43.0009° |
| perigee height: | 533 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 21.1588° |
| argument of perigee: | 232.7440° |
| revolutions per day: | 15.09710925 |
| mean anomaly at epoch: | 127.2919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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