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 28158U 26106.31850242 +.00000000 +00000-0 +00000-0 0 00007
2 28158 11.9797 26.5206 0001869 292.0330 281.2028 1.00427046 01
| Epoch (UTC): | 16 April 2026 07:38:38 |
| Eccentricity: | 0.0001869 |
| inclination: | 11.9797° |
| perigee height: | 35735 km |
| apogee height: | 35751 km |
| right ascension of ascending node: | 26.5206° |
| argument of perigee: | 292.0330° |
| revolutions per day: | 1.00427046 |
| mean anomaly at epoch: | 281.2028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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