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 49082U 26145.33179906 +.00000000 +00000-0 -83958-4 0 00000
2 49082 87.9152 10.4107 0001667 87.1524 272.9799 13.17650817 01
| Epoch (UTC): | 25 May 2026 07:57:47 |
| Eccentricity: | 0.0001667 |
| inclination: | 87.9152° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4107° |
| argument of perigee: | 87.1524° |
| revolutions per day: | 13.17650817 |
| mean anomaly at epoch: | 272.9799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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