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 04420U 26044.70008929 +.00000000 +00000-0 +28995-4 0 00001
2 04420 81.2305 117.8443 0085942 260.6497 98.4950 14.12603717 08
| Epoch (UTC): | 13 February 2026 16:48:07 |
| Eccentricity: | 0.0085942 |
| inclination: | 81.2305° |
| perigee height: | 788 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 117.8443° |
| argument of perigee: | 260.6497° |
| revolutions per day: | 14.12603717 |
| mean anomaly at epoch: | 98.4950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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