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 26049.83347841 +.00000000 +00000-0 +11118-4 0 00009
2 19650 70.9994 191.1684 0012939 31.2043 328.9845 14.16152042 03
| Epoch (UTC): | 18 February 2026 20:00:12 |
| Eccentricity: | 0.0012939 |
| inclination: | 70.9994° |
| perigee height: | 829 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 191.1684° |
| argument of perigee: | 31.2043° |
| revolutions per day: | 14.16152042 |
| mean anomaly at epoch: | 328.9845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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