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 49093U 26145.38073262 +.00000000 +00000-0 +98698-4 0 00001
2 49093 87.9161 10.3885 0002109 93.9790 266.1582 13.17650899 02
| Epoch (UTC): | 25 May 2026 09:08:15 |
| Eccentricity: | 0.0002109 |
| inclination: | 87.9161° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3885° |
| argument of perigee: | 93.9790° |
| revolutions per day: | 13.17650899 |
| mean anomaly at epoch: | 266.1582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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