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 28892U 05043C 23339.35409469 .00002264 00000-0 41857-3 0 9993
2 28892 98.1829 110.6255 0014550 253.3252 106.6354 14.66316375965956
| Epoch (UTC): | 05 December 2023 08:29:53 |
| Eccentricity: | 0.0014550 |
| inclination: | 98.1829° |
| perigee height: | 662 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 110.6255° |
| argument of perigee: | 253.3252° |
| revolutions per day: | 14.66316375 |
| mean anomaly at epoch: | 106.6354° |
| orbit number at epoch: | 96595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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