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 29658U 06060A 21053.77244420 0.00000700 00000-0 26048-4 0 07
2 29658 98.1600 249.2284 0003005 353.7748 6.2251 15.27524611 02
| Epoch (UTC): | 22 February 2021 18:32:19 |
| Eccentricity: | 0.0003005 |
| inclination: | 98.1600° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 249.2284° |
| argument of perigee: | 353.7748° |
| revolutions per day: | 15.27524611 |
| mean anomaly at epoch: | 6.2251° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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