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 27843U 26087.88816941 +.00000000 +00000-0 +70086-4 0 00000
2 27843 98.7079 96.7262 0010823 121.1901 239.0339 14.21304418 04
| Epoch (UTC): | 28 March 2026 21:18:57 |
| Eccentricity: | 0.0010823 |
| inclination: | 98.7079° |
| perigee height: | 813 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 96.7262° |
| argument of perigee: | 121.1901° |
| revolutions per day: | 14.21304418 |
| mean anomaly at epoch: | 239.0339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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