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 23028.05400533 .00000986 00000-0 17520-3 0 9995
2 29 48.3794 122.3595 0023877 356.1032 3.9690 14.74956606359521
| Epoch (UTC): | 28 January 2023 01:17:46 |
| Eccentricity: | 0.0023877 |
| inclination: | 48.3794° |
| perigee height: | 628 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 122.3595° |
| argument of perigee: | 356.1032° |
| revolutions per day: | 14.74956606 |
| mean anomaly at epoch: | 3.9690° |
| orbit number at epoch: | 35952 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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