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 26039.80330508 +.00000000 +00000-0 +14138-3 0 00001
2 19650 70.9973 212.2725 0012457 49.2592 310.9611 14.16147168 09
| Epoch (UTC): | 08 February 2026 19:16:45 |
| Eccentricity: | 0.0012457 |
| inclination: | 70.9973° |
| perigee height: | 829 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 212.2725° |
| argument of perigee: | 49.2592° |
| revolutions per day: | 14.16147168 |
| mean anomaly at epoch: | 310.9611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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