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 data is extracted from the following two-line orbital elements,
1 116U 61015A 23334.50242237 .00000145 00000-0 16914-3 0 9995
2 116 66.8107 5.0992 0078817 209.4222 150.2410 13.91973498167792
| Epoch (UTC): | 30 November 2023 12:03:29 |
| Eccentricity: | 0.0078817 |
| inclination: | 66.8107° |
| perigee height: | 864 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 5.0992° |
| argument of perigee: | 209.4222° |
| revolutions per day: | 13.91973498 |
| mean anomaly at epoch: | 150.2410° |
| orbit number at epoch: | 16779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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