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 49000U 26145.52533987 +.00000000 +00000-0 -16887-4 0 00001
2 49000 87.9102 233.2796 0001841 100.8083 259.3256 13.16595583 06
| Epoch (UTC): | 25 May 2026 12:36:29 |
| Eccentricity: | 0.0001841 |
| inclination: | 87.9102° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2796° |
| argument of perigee: | 100.8083° |
| revolutions per day: | 13.16595583 |
| mean anomaly at epoch: | 259.3256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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