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 23081.12350778 .00000109 00000-0 11784-3 0 9991
2 00005 34.2562 3.6397 1846431 207.5915 141.3424 10.85073303314707
| Epoch (UTC): | 22 March 2023 02:57:51 |
| Eccentricity: | 0.1846431 |
| inclination: | 34.2562° |
| perigee height: | 649 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 3.6397° |
| argument of perigee: | 207.5915° |
| revolutions per day: | 10.85073303 |
| mean anomaly at epoch: | 141.3424° |
| orbit number at epoch: | 31470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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