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 38858U 12055B 23336.46599026 .00000050 00000-0 00000-0 0 9998
2 38858 55.3224 127.0434 0001530 159.1066 200.8720 1.70473897 69193
| Epoch (UTC): | 02 December 2023 11:11:01 |
| Eccentricity: | 0.0001530 |
| inclination: | 55.3224° |
| perigee height: | 23217 km |
| apogee height: | 23226 km |
| right ascension of ascending node: | 127.0434° |
| argument of perigee: | 159.1066° |
| revolutions per day: | 1.70473897 |
| mean anomaly at epoch: | 200.8720° |
| orbit number at epoch: | 6919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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