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 57610U 26145.34123153 +.00000000 +00000-0 +14369-4 0 00009
2 57610 43.0041 8.3126 0001397 260.3039 99.7655 15.27578289 01
| Epoch (UTC): | 25 May 2026 08:11:22 |
| Eccentricity: | 0.0001397 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.3126° |
| argument of perigee: | 260.3039° |
| revolutions per day: | 15.27578289 |
| mean anomaly at epoch: | 99.7655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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