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 26066.59677279 +.00000000 +00000-0 +23007-3 0 00005
2 27844 98.6780 76.4215 0010613 117.8292 242.3964 14.24264289 03
| Epoch (UTC): | 07 March 2026 14:19:21 |
| Eccentricity: | 0.0010613 |
| inclination: | 98.6780° |
| perigee height: | 803 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 76.4215° |
| argument of perigee: | 117.8292° |
| revolutions per day: | 14.24264289 |
| mean anomaly at epoch: | 242.3964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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