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 46278U 26145.60885867 +.00000000 +00000-0 +28459-3 0 00007
2 46278 97.2108 230.0178 0002714 121.5002 238.6526 15.69608944 06
| Epoch (UTC): | 25 May 2026 14:36:45 |
| Eccentricity: | 0.0002714 |
| inclination: | 97.2108° |
| perigee height: | 358 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 230.0178° |
| argument of perigee: | 121.5002° |
| revolutions per day: | 15.69608944 |
| mean anomaly at epoch: | 238.6526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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