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 40019U 26053.63142455 +.00000000 +00000-0 +11198-3 0 00006
2 40019 97.9456 183.2797 0077689 279.7786 79.4654 14.70721906 08
| Epoch (UTC): | 22 February 2026 15:09:15 |
| Eccentricity: | 0.0077689 |
| inclination: | 97.9456° |
| perigee height: | 604 km |
| apogee height: | 713 km |
| right ascension of ascending node: | 183.2797° |
| argument of perigee: | 279.7786° |
| revolutions per day: | 14.70721906 |
| mean anomaly at epoch: | 79.4654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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