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 28932U 06002B 23339.21463041 .00005609 00000-0 44621-3 0 9993
2 28932 98.2243 55.2380 0079666 127.7513 233.0960 14.98353948970112
| Epoch (UTC): | 05 December 2023 05:09:04 |
| Eccentricity: | 0.0079666 |
| inclination: | 98.2243° |
| perigee height: | 516 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 55.2380° |
| argument of perigee: | 127.7513° |
| revolutions per day: | 14.98353948 |
| mean anomaly at epoch: | 233.0960° |
| orbit number at epoch: | 97011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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