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 22698U 26053.80618639 +.00000000 +00000-0 +50051-4 0 00002
2 22698 89.4926 66.8852 0087410 199.0678 160.7237 14.24155075 02
| Epoch (UTC): | 22 February 2026 19:20:54 |
| Eccentricity: | 0.0087410 |
| inclination: | 89.4926° |
| perigee height: | 748 km |
| apogee height: | 874 km |
| right ascension of ascending node: | 66.8852° |
| argument of perigee: | 199.0678° |
| revolutions per day: | 14.24155075 |
| mean anomaly at epoch: | 160.7237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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