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 42063U 26108.97670463 +.00000000 +00000-0 -97600-5 0 00005
2 42063 98.5660 184.5917 0001259 93.8200 266.3127 14.30820989 06
| Epoch (UTC): | 18 April 2026 23:26:27 |
| Eccentricity: | 0.0001259 |
| inclination: | 98.5660° |
| perigee height: | 788 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 184.5917° |
| argument of perigee: | 93.8200° |
| revolutions per day: | 14.30820989 |
| mean anomaly at epoch: | 266.3127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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