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 26065.47274804 +.00000000 +00000-0 +22533-3 0 00001
2 27844 98.6780 75.3114 0010574 120.8066 239.4155 14.24263129 09
| Epoch (UTC): | 06 March 2026 11:20:45 |
| Eccentricity: | 0.0010574 |
| inclination: | 98.6780° |
| perigee height: | 803 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 75.3114° |
| argument of perigee: | 120.8066° |
| revolutions per day: | 14.24263129 |
| mean anomaly at epoch: | 239.4155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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