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 61555U 26145.63096286 +.00000000 +00000-0 +11703-3 0 00008
2 61555 88.9832 61.2780 0005014 196.7184 163.3822 13.86382066 00
| Epoch (UTC): | 25 May 2026 15:08:35 |
| Eccentricity: | 0.0005014 |
| inclination: | 88.9832° |
| perigee height: | 938 km |
| apogee height: | 945 km |
| right ascension of ascending node: | 61.2780° |
| argument of perigee: | 196.7184° |
| revolutions per day: | 13.86382066 |
| mean anomaly at epoch: | 163.3822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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