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 22279.04546675 .00000254 00000-0 31147-3 0 9999
2 00005 34.2447 158.5779 1846424 175.3560 186.7054 10.85016090296557
| Epoch (UTC): | 06 October 2022 01:05:28 |
| Eccentricity: | 0.1846424 |
| inclination: | 34.2447° |
| perigee height: | 649 km |
| apogee height: | 3832 km |
| right ascension of ascending node: | 158.5779° |
| argument of perigee: | 175.3560° |
| revolutions per day: | 10.85016090 |
| mean anomaly at epoch: | 186.7054° |
| orbit number at epoch: | 29655 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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