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 28061U 26131.91289163 +.00000000 +00000-0 -10124-3 0 00004
2 28061 99.5464 167.5240 0145164 294.0396 64.5632 13.97750587 03
| Epoch (UTC): | 11 May 2026 21:54:33 |
| Eccentricity: | 0.0145164 |
| inclination: | 99.5464° |
| perigee height: | 796 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 167.5240° |
| argument of perigee: | 294.0396° |
| revolutions per day: | 13.97750587 |
| mean anomaly at epoch: | 64.5632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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