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 26129.42760946 +.00000000 +00000-0 +15625-3 0 00001
2 00107 28.7749 179.9024 0494204 126.3499 238.3726 14.21978872 06
| Epoch (UTC): | 09 May 2026 10:15:45 |
| Eccentricity: | 0.0494204 |
| inclination: | 28.7749° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 179.9024° |
| argument of perigee: | 126.3499° |
| revolutions per day: | 14.21978872 |
| mean anomaly at epoch: | 238.3726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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