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 23152.39865962 .00000255 00000-0 91941-4 0 9995
2 05175 74.0464 165.9060 0030184 198.0726 161.9358 14.38359657727348
| Epoch (UTC): | 01 June 2023 09:34:04 |
| Eccentricity: | 0.0030184 |
| inclination: | 74.0464° |
| perigee height: | 742 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 165.9060° |
| argument of perigee: | 198.0726° |
| revolutions per day: | 14.38359657 |
| mean anomaly at epoch: | 161.9358° |
| orbit number at epoch: | 72734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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