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 23337.16170026 .00000365 00000-0 21937-3 0 9999
2 28654 98.8957 50.6184 0013341 260.4910 99.4754 14.13070194955435
| Epoch (UTC): | 03 December 2023 03:52:50 |
| Eccentricity: | 0.0013341 |
| inclination: | 98.8957° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 50.6184° |
| argument of perigee: | 260.4910° |
| revolutions per day: | 14.13070194 |
| mean anomaly at epoch: | 99.4754° |
| orbit number at epoch: | 95543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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