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 19650U 26041.49854939 +.00000000 +00000-0 +17637-3 0 00005
2 19650 70.9976 208.7055 0012545 46.3746 313.8415 14.16148229 08
| Epoch (UTC): | 10 February 2026 11:57:54 |
| Eccentricity: | 0.0012545 |
| inclination: | 70.9976° |
| perigee height: | 829 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 208.7055° |
| argument of perigee: | 46.3746° |
| revolutions per day: | 14.16148229 |
| mean anomaly at epoch: | 313.8415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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