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 28485U 04047A 22343.73736454 .00004370 00000-0 24865-3 0 9997
2 28485 20.5550 158.8402 0010340 4.6858 355.3672 15.07702568990104
| Epoch (UTC): | 09 December 2022 17:41:48 |
| Eccentricity: | 0.0010340 |
| inclination: | 20.5550° |
| perigee height: | 536 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 158.8402° |
| argument of perigee: | 4.6858° |
| revolutions per day: | 15.07702568 |
| mean anomaly at epoch: | 355.3672° |
| orbit number at epoch: | 99010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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