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 23340.39961482 .00001169 00000-0 19830-3 0 9994
2 29 48.3792 85.9143 0024187 257.0025 102.8186 14.75790076405640
| Epoch (UTC): | 06 December 2023 09:35:26 |
| Eccentricity: | 0.0024187 |
| inclination: | 48.3792° |
| perigee height: | 625 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 85.9143° |
| argument of perigee: | 257.0025° |
| revolutions per day: | 14.75790076 |
| mean anomaly at epoch: | 102.8186° |
| orbit number at epoch: | 40564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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