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 22824U 26145.64214016 +.00000000 +00000-0 -34051-5 0 00002
2 22824 98.7735 209.8116 0005468 309.0244 216.8179 14.27469686 08
| Epoch (UTC): | 25 May 2026 15:24:40 |
| Eccentricity: | 0.0005468 |
| inclination: | 98.7735° |
| perigee height: | 796 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 209.8116° |
| argument of perigee: | 309.0244° |
| revolutions per day: | 14.27469686 |
| mean anomaly at epoch: | 216.8179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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