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 24284.53546278 .00000898 00000-0 50107-3 0 9990
2 28654 98.8661 0.5055 0015230 96.7931 263.4974 14.13365965999461
| Epoch (UTC): | 10 October 2024 12:51:03 |
| Eccentricity: | 0.0015230 |
| inclination: | 98.8661° |
| perigee height: | 837 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 0.5055° |
| argument of perigee: | 96.7931° |
| revolutions per day: | 14.13365965 |
| mean anomaly at epoch: | 263.4974° |
| orbit number at epoch: | 99946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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