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 22803U 26044.47925463 +.00000000 +00000-0 -31863-4 0 00000
2 22803 70.9890 62.1824 0019461 249.9138 109.9892 14.17228174 05
| Epoch (UTC): | 13 February 2026 11:30:07 |
| Eccentricity: | 0.0019461 |
| inclination: | 70.9890° |
| perigee height: | 821 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 62.1824° |
| argument of perigee: | 249.9138° |
| revolutions per day: | 14.17228174 |
| mean anomaly at epoch: | 109.9892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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