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 31807U 99025CGV 23037.83152565 .00002520 00000-0 71810-3 0 9993
2 31807 99.1082 85.2250 0122885 18.2036 342.3492 14.41903955502722
| Epoch (UTC): | 06 February 2023 19:57:23 |
| Eccentricity: | 0.0122885 |
| inclination: | 99.1082° |
| perigee height: | 664 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 85.2250° |
| argument of perigee: | 18.2036° |
| revolutions per day: | 14.41903955 |
| mean anomaly at epoch: | 342.3492° |
| orbit number at epoch: | 50272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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