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 24358.15694813 .00000416 00000-0 24437-3 0 9992
2 28654 98.8599 73.4345 0013390 245.4212 114.5566 14.13460391 9950
| Epoch (UTC): | 23 December 2024 03:46:00 |
| Eccentricity: | 0.0013390 |
| inclination: | 98.8599° |
| perigee height: | 838 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 73.4345° |
| argument of perigee: | 245.4212° |
| revolutions per day: | 14.13460391 |
| mean anomaly at epoch: | 114.5566° |
| orbit number at epoch: | 995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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