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 61197U 26145.59254963 +.00000000 +00000-0 +12210-3 0 00007
2 61197 44.8616 238.1007 0007705 320.9859 39.0415 13.99131349 06
| Epoch (UTC): | 25 May 2026 14:13:16 |
| Eccentricity: | 0.0007705 |
| inclination: | 44.8616° |
| perigee height: | 891 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 238.1007° |
| argument of perigee: | 320.9859° |
| revolutions per day: | 13.99131349 |
| mean anomaly at epoch: | 39.0415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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