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 24255.88844715 .00004020 00000-0 59413-3 0 9993
2 29 48.3764 198.2712 0022963 19.3366 340.8413 14.76789598447085
| Epoch (UTC): | 11 September 2024 21:19:21 |
| Eccentricity: | 0.0022963 |
| inclination: | 48.3764° |
| perigee height: | 623 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 198.2712° |
| argument of perigee: | 19.3366° |
| revolutions per day: | 14.76789598 |
| mean anomaly at epoch: | 340.8413° |
| orbit number at epoch: | 44708 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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