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 36089U 26019.15727225 +.00000000 +00000-0 +74658-4 0 00002
2 36089 98.4393 355.9155 0078816 136.5777 224.1663 14.52258872 01
| Epoch (UTC): | 19 January 2026 03:46:28 |
| Eccentricity: | 0.0078816 |
| inclination: | 98.4393° |
| perigee height: | 662 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 355.9155° |
| argument of perigee: | 136.5777° |
| revolutions per day: | 14.52258872 |
| mean anomaly at epoch: | 224.1663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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