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 05175U 71035B 23156.43266393 .00000220 00000-0 80498-4 0 9994
2 05175 74.0463 158.4774 0030018 189.7346 170.3231 14.38361835727926
| Epoch (UTC): | 05 June 2023 10:23:02 |
| Eccentricity: | 0.0030018 |
| inclination: | 74.0463° |
| perigee height: | 742 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 158.4774° |
| argument of perigee: | 189.7346° |
| revolutions per day: | 14.38361835 |
| mean anomaly at epoch: | 170.3231° |
| orbit number at epoch: | 72792 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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