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 29228U 06021A 24263.49623038 .00004789 00000-0 31527-3 0 9993
2 29228 69.9359 179.7193 0007184 243.0105 117.0325 15.08197923 6569
| Epoch (UTC): | 19 September 2024 11:54:34 |
| Eccentricity: | 0.0007184 |
| inclination: | 69.9359° |
| perigee height: | 537 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 179.7193° |
| argument of perigee: | 243.0105° |
| revolutions per day: | 15.08197923 |
| mean anomaly at epoch: | 117.0325° |
| orbit number at epoch: | 656 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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