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 14077U 26150.35290506 +.00000000 +00000-0 +00000-0 0 00006
2 14077 12.4779 333.7577 0038216 357.1215 5.4638 0.99161951 07
| Epoch (UTC): | 30 May 2026 08:28:10 |
| Eccentricity: | 0.0038216 |
| inclination: | 12.4779° |
| perigee height: | 35938 km |
| apogee height: | 36263 km |
| right ascension of ascending node: | 333.7577° |
| argument of perigee: | 357.1215° |
| revolutions per day: | 0.99161951 |
| mean anomaly at epoch: | 5.4638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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