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 26041.85172508 +.00000000 +00000-0 +18123-3 0 00001
2 19650 70.9978 207.9623 0012560 45.7314 314.4838 14.16148449 03
| Epoch (UTC): | 10 February 2026 20:26:29 |
| Eccentricity: | 0.0012560 |
| inclination: | 70.9978° |
| perigee height: | 829 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 207.9623° |
| argument of perigee: | 45.7314° |
| revolutions per day: | 14.16148449 |
| mean anomaly at epoch: | 314.4838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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