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 23336.47267695 .00003381 00000-0 51600-3 0 9992
2 00029 48.3772 104.4885 0024072 240.5888 119.2621 14.75783563404957
| Epoch (UTC): | 02 December 2023 11:20:39 |
| Eccentricity: | 0.0024072 |
| inclination: | 48.3772° |
| perigee height: | 626 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 104.4885° |
| argument of perigee: | 240.5888° |
| revolutions per day: | 14.75783563 |
| mean anomaly at epoch: | 119.2621° |
| orbit number at epoch: | 40495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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