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 49108U 26145.34883196 +.00000000 +00000-0 -22066-4 0 00006
2 49108 87.9155 10.4306 0001745 92.3598 267.7733 13.17648596 01
| Epoch (UTC): | 25 May 2026 08:22:19 |
| Eccentricity: | 0.0001745 |
| inclination: | 87.9155° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4306° |
| argument of perigee: | 92.3598° |
| revolutions per day: | 13.17648596 |
| mean anomaly at epoch: | 267.7733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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