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 23027.47899706 .00000281 00000-0 10060-3 0 9999
2 05175 74.0480 35.9175 0028435 96.8590 263.5801 14.38234291709381
| Epoch (UTC): | 27 January 2023 11:29:45 |
| Eccentricity: | 0.0028435 |
| inclination: | 74.0480° |
| perigee height: | 744 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 35.9175° |
| argument of perigee: | 96.8590° |
| revolutions per day: | 14.38234291 |
| mean anomaly at epoch: | 263.5801° |
| orbit number at epoch: | 70938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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