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 26133.35802421 +.00000000 +00000-0 +12591-3 0 00002
2 00107 28.7758 157.2430 0494118 163.0363 198.7384 14.21986862 05
| Epoch (UTC): | 13 May 2026 08:35:33 |
| Eccentricity: | 0.0494118 |
| inclination: | 28.7758° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 157.2430° |
| argument of perigee: | 163.0363° |
| revolutions per day: | 14.21986862 |
| mean anomaly at epoch: | 198.7384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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