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 22828U 26053.69636262 +.00000000 +00000-0 +70650-4 0 00003
2 22828 98.6992 120.9051 0010178 29.3075 330.8677 14.31753968 09
| Epoch (UTC): | 22 February 2026 16:42:45 |
| Eccentricity: | 0.0010178 |
| inclination: | 98.6992° |
| perigee height: | 779 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 120.9051° |
| argument of perigee: | 29.3075° |
| revolutions per day: | 14.31753968 |
| mean anomaly at epoch: | 330.8677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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