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 26037.61361245 +.00000000 +00000-0 +73165-4 0 00006
2 19650 70.9970 216.8800 0012346 52.9971 307.2280 14.16146329 08
| Epoch (UTC): | 06 February 2026 14:43:36 |
| Eccentricity: | 0.0012346 |
| inclination: | 70.9970° |
| perigee height: | 830 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 216.8800° |
| argument of perigee: | 52.9971° |
| revolutions per day: | 14.16146329 |
| mean anomaly at epoch: | 307.2280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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