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 29499U 06044A 21125.39257243 -.00000000 00000-0 19104-4 0 9993
2 29499 98.4763 166.3725 0001734 82.9720 338.4073 14.21497556754621
| Epoch (UTC): | 05 May 2021 09:25:18 |
| Eccentricity: | 0.0001734 |
| inclination: | 98.4763° |
| perigee height: | 819 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 166.3725° |
| argument of perigee: | 82.9720° |
| revolutions per day: | 14.21497556 |
| mean anomaly at epoch: | 338.4073° |
| orbit number at epoch: | 75462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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