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 18749U 26017.14346984 +.00000000 +00000-0 +38275-4 0 00006
2 18749 82.5112 243.8485 0019292 51.7889 308.5060 14.85462997 02
| Epoch (UTC): | 17 January 2026 03:26:35 |
| Eccentricity: | 0.0019292 |
| inclination: | 82.5112° |
| perigee height: | 599 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 243.8485° |
| argument of perigee: | 51.7889° |
| revolutions per day: | 14.85462997 |
| mean anomaly at epoch: | 308.5060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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