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 49098U 26145.33011825 +.00000000 +00000-0 +10176-3 0 00002
2 49098 87.9153 10.4193 0001858 94.8056 265.3287 13.17649633 03
| Epoch (UTC): | 25 May 2026 07:55:22 |
| Eccentricity: | 0.0001858 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4193° |
| argument of perigee: | 94.8056° |
| revolutions per day: | 13.17649633 |
| mean anomaly at epoch: | 265.3287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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