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 49106U 26145.55082021 +.00000000 +00000-0 +58138-4 0 00003
2 49106 87.8961 355.1507 0002312 92.9194 267.2199 13.12443038 04
| Epoch (UTC): | 25 May 2026 13:13:10 |
| Eccentricity: | 0.0002312 |
| inclination: | 87.8961° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1507° |
| argument of perigee: | 92.9194° |
| revolutions per day: | 13.12443038 |
| mean anomaly at epoch: | 267.2199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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