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 00005U 58002B 23029.66605721 .00000138 00000-0 17454-3 0 9995
2 00005 34.2486 162.2556 1845960 335.8478 16.5322 10.85056100309111
| Epoch (UTC): | 29 January 2023 15:59:07 |
| Eccentricity: | 0.1845960 |
| inclination: | 34.2486° |
| perigee height: | 649 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 162.2556° |
| argument of perigee: | 335.8478° |
| revolutions per day: | 10.85056100 |
| mean anomaly at epoch: | 16.5322° |
| orbit number at epoch: | 30911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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