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 50316U 82092AAH 23062.77529987 .20683930 -11663-5 11210-2 0 9994
2 50316 82.4793 4.8766 0012489 194.9198 165.1735 16.41251766 68681
| Epoch (UTC): | 03 March 2023 18:36:25 |
| Eccentricity: | 0.0012489 |
| inclination: | 82.4793° |
| perigee height: | 154 km |
| apogee height: | 170 km |
| right ascension of ascending node: | 4.8766° |
| argument of perigee: | 194.9198° |
| revolutions per day: | 16.41251766 |
| mean anomaly at epoch: | 165.1735° |
| orbit number at epoch: | 6868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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