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 26039.02631757 +.00000000 +00000-0 +12048-3 0 00003
2 19650 70.9971 213.9074 0012421 50.5752 309.6468 14.16146823 08
| Epoch (UTC): | 08 February 2026 00:37:53 |
| Eccentricity: | 0.0012421 |
| inclination: | 70.9971° |
| perigee height: | 829 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 213.9074° |
| argument of perigee: | 50.5752° |
| revolutions per day: | 14.16146823 |
| mean anomaly at epoch: | 309.6468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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