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 23151.49448535 .00000245 00000-0 88555-4 0 9994
2 05175 74.0464 167.5709 0030233 199.9376 160.0599 14.38359106727214
| Epoch (UTC): | 31 May 2023 11:52:03 |
| Eccentricity: | 0.0030233 |
| inclination: | 74.0464° |
| perigee height: | 742 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 167.5709° |
| argument of perigee: | 199.9376° |
| revolutions per day: | 14.38359106 |
| mean anomaly at epoch: | 160.0599° |
| orbit number at epoch: | 72721 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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