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 49060U 26145.63032148 +.00000000 +00000-0 +11362-3 0 00003
2 49060 89.0055 220.9192 0005086 162.6594 197.4757 13.94716696 07
| Epoch (UTC): | 25 May 2026 15:07:39 |
| Eccentricity: | 0.0005086 |
| inclination: | 89.0055° |
| perigee height: | 908 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 220.9192° |
| argument of perigee: | 162.6594° |
| revolutions per day: | 13.94716696 |
| mean anomaly at epoch: | 197.4757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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