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 49810U 26143.16836868 +.00000000 +00000-0 +00000-0 0 00007
2 49810 57.1703 342.3482 0000531 126.1506 231.6723 1.70475835 07
| Epoch (UTC): | 23 May 2026 04:02:27 |
| Eccentricity: | 0.0000531 |
| inclination: | 57.1703° |
| perigee height: | 23220 km |
| apogee height: | 23224 km |
| right ascension of ascending node: | 342.3482° |
| argument of perigee: | 126.1506° |
| revolutions per day: | 1.70475835 |
| mean anomaly at epoch: | 231.6723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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