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 28654U 05018A 23333.40890854 .00000440 00000-0 25950-3 0 9993
2 28654 98.8960 46.8894 0013316 272.0287 87.9360 14.13066469954908
| Epoch (UTC): | 29 November 2023 09:48:49 |
| Eccentricity: | 0.0013316 |
| inclination: | 98.8960° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 46.8894° |
| argument of perigee: | 272.0287° |
| revolutions per day: | 14.13066469 |
| mean anomaly at epoch: | 87.9360° |
| orbit number at epoch: | 95490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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