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 26073.54634750 +.00000000 +00000-0 +44426-3 0 00006
2 00107 28.7764 141.9952 0494383 324.5714 32.2951 14.21778093 06
| Epoch (UTC): | 14 March 2026 13:06:44 |
| Eccentricity: | 0.0494383 |
| inclination: | 28.7764° |
| perigee height: | 464 km |
| apogee height: | 1175 km |
| right ascension of ascending node: | 141.9952° |
| argument of perigee: | 324.5714° |
| revolutions per day: | 14.21778093 |
| mean anomaly at epoch: | 32.2951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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