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 26074.95667745 +.00000000 +00000-0 +16452-3 0 00007
2 27844 98.6777 84.6777 0010762 96.1930 264.0475 14.24271605 04
| Epoch (UTC): | 15 March 2026 22:57:36 |
| Eccentricity: | 0.0010762 |
| inclination: | 98.6777° |
| perigee height: | 803 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 84.6777° |
| argument of perigee: | 96.1930° |
| revolutions per day: | 14.24271605 |
| mean anomaly at epoch: | 264.0475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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