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 29U 60002B 23030.42504971 .00000621 00000-0 12166-3 0 9997
2 29 48.3795 111.1593 0023778 6.2794 353.8412 14.74960398359885
| Epoch (UTC): | 30 January 2023 10:12:04 |
| Eccentricity: | 0.0023778 |
| inclination: | 48.3795° |
| perigee height: | 628 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 111.1593° |
| argument of perigee: | 6.2794° |
| revolutions per day: | 14.74960398 |
| mean anomaly at epoch: | 353.8412° |
| orbit number at epoch: | 35988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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