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 27844U 26066.24551513 +.00000000 +00000-0 +23549-3 0 00000
2 27844 98.6780 76.0746 0010602 118.7585 241.4660 14.24264005 00
| Epoch (UTC): | 07 March 2026 05:53:32 |
| Eccentricity: | 0.0010602 |
| inclination: | 98.6780° |
| perigee height: | 803 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 76.0746° |
| argument of perigee: | 118.7585° |
| revolutions per day: | 14.24264005 |
| mean anomaly at epoch: | 241.4660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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