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 00107U 26083.65745118 +.00000000 +00000-0 +28684-3 0 00008
2 00107 28.7741 83.7213 0494413 59.0045 305.8143 14.21826158 03
| Epoch (UTC): | 24 March 2026 15:46:43 |
| Eccentricity: | 0.0494413 |
| inclination: | 28.7741° |
| perigee height: | 463 km |
| apogee height: | 1175 km |
| right ascension of ascending node: | 83.7213° |
| argument of perigee: | 59.0045° |
| revolutions per day: | 14.21826158 |
| mean anomaly at epoch: | 305.8143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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