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 26072.98964530 +.00000000 +00000-0 +19032-3 0 00007
2 27844 98.6777 82.7351 0010745 101.3524 258.8862 14.24270180 08
| Epoch (UTC): | 13 March 2026 23:45:05 |
| Eccentricity: | 0.0010745 |
| inclination: | 98.6777° |
| perigee height: | 803 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 82.7351° |
| argument of perigee: | 101.3524° |
| revolutions per day: | 14.24270180 |
| mean anomaly at epoch: | 258.8862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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