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 61192U 26145.59078758 +.00000000 +00000-0 +26225-3 0 00009
2 61192 97.5520 234.8326 0012811 349.3571 10.7384 15.08673586 04
| Epoch (UTC): | 25 May 2026 14:10:44 |
| Eccentricity: | 0.0012811 |
| inclination: | 97.5520° |
| perigee height: | 531 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 234.8326° |
| argument of perigee: | 349.3571° |
| revolutions per day: | 15.08673586 |
| mean anomaly at epoch: | 10.7384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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