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 40057U 26018.94612285 +.00000000 +00000-0 +49792-3 0 00007
2 40057 98.2697 275.5598 0009190 48.5319 311.6688 14.96091394 08
| Epoch (UTC): | 18 January 2026 22:42:25 |
| Eccentricity: | 0.0009190 |
| inclination: | 98.2697° |
| perigee height: | 573 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 275.5598° |
| argument of perigee: | 48.5319° |
| revolutions per day: | 14.96091394 |
| mean anomaly at epoch: | 311.6688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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