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 26110.19162553 +.00000000 +00000-0 +11326-3 0 00009
2 00107 28.7796 290.7895 0494165 306.7757 48.8429 14.21925021 05
| Epoch (UTC): | 20 April 2026 04:35:56 |
| Eccentricity: | 0.0494165 |
| inclination: | 28.7796° |
| perigee height: | 463 km |
| apogee height: | 1175 km |
| right ascension of ascending node: | 290.7895° |
| argument of perigee: | 306.7757° |
| revolutions per day: | 14.21925021 |
| mean anomaly at epoch: | 48.8429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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