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 42113U 26017.70537007 +.00000000 +00000-0 +11574-2 0 00009
2 42113 82.7489 350.2058 0195092 24.6700 153.8320 13.73495970 09
| Epoch (UTC): | 17 January 2026 16:55:43 |
| Eccentricity: | 0.0195092 |
| inclination: | 82.7489° |
| perigee height: | 843 km |
| apogee height: | 1131 km |
| right ascension of ascending node: | 350.2058° |
| argument of perigee: | 24.6700° |
| revolutions per day: | 13.73495970 |
| mean anomaly at epoch: | 153.8320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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