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 49105U 26145.31660605 +.00000000 +00000-0 +16823-3 0 00000
2 49105 87.9151 10.4164 0002353 86.3583 273.7818 13.17651715 07
| Epoch (UTC): | 25 May 2026 07:35:54 |
| Eccentricity: | 0.0002353 |
| inclination: | 87.9151° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4164° |
| argument of perigee: | 86.3583° |
| revolutions per day: | 13.17651715 |
| mean anomaly at epoch: | 273.7818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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