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 26106.43224874 +.00000000 +00000-0 +42206-4 0 00007
2 22698 89.4992 63.8501 0089410 29.6365 330.9850 14.24171615 06
| Epoch (UTC): | 16 April 2026 10:22:26 |
| Eccentricity: | 0.0089410 |
| inclination: | 89.4992° |
| perigee height: | 747 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 63.8501° |
| argument of perigee: | 29.6365° |
| revolutions per day: | 14.24171615 |
| mean anomaly at epoch: | 330.9850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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