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 49216U 26145.47648387 +.00000000 +00000-0 +71359-3 0 00008
2 49216 87.8942 324.7573 0001367 89.3831 270.7455 13.13469206 07
| Epoch (UTC): | 25 May 2026 11:26:08 |
| Eccentricity: | 0.0001367 |
| inclination: | 87.8942° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7573° |
| argument of perigee: | 89.3831° |
| revolutions per day: | 13.13469206 |
| mean anomaly at epoch: | 270.7455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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