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 00029U 60002B 23335.59249893 .00002099 00000-0 33192-3 0 9995
2 00029 48.3779 108.6517 0024064 236.8419 123.0185 14.75774707404825
| Epoch (UTC): | 01 December 2023 14:13:11 |
| Eccentricity: | 0.0024064 |
| inclination: | 48.3779° |
| perigee height: | 626 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 108.6517° |
| argument of perigee: | 236.8419° |
| revolutions per day: | 14.75774707 |
| mean anomaly at epoch: | 123.0185° |
| orbit number at epoch: | 40482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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