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 22829U 26100.15937522 +.00000000 +00000-0 +50630-4 0 00007
2 22829 98.6702 167.3134 0008900 224.7581 135.2884 14.31900058 00
| Epoch (UTC): | 10 April 2026 03:49:30 |
| Eccentricity: | 0.0008900 |
| inclination: | 98.6702° |
| perigee height: | 779 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 167.3134° |
| argument of perigee: | 224.7581° |
| revolutions per day: | 14.31900058 |
| mean anomaly at epoch: | 135.2884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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