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 49107U 26145.32504873 +.00000000 +00000-0 +94805-4 0 00004
2 49107 87.9155 10.4155 0001852 89.3239 270.8105 13.17650815 04
| Epoch (UTC): | 25 May 2026 07:48:04 |
| Eccentricity: | 0.0001852 |
| inclination: | 87.9155° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4155° |
| argument of perigee: | 89.3239° |
| revolutions per day: | 13.17650815 |
| mean anomaly at epoch: | 270.8105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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