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 49809U 26142.76935786 +.00000000 +00000-0 +00000-0 0 00009
2 49809 57.1681 342.3603 0000787 191.0979 169.2233 1.70475764 06
| Epoch (UTC): | 22 May 2026 18:27:52 |
| Eccentricity: | 0.0000787 |
| inclination: | 57.1681° |
| perigee height: | 23220 km |
| apogee height: | 23224 km |
| right ascension of ascending node: | 342.3603° |
| argument of perigee: | 191.0979° |
| revolutions per day: | 1.70475764 |
| mean anomaly at epoch: | 169.2233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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