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 29241U 06024B 20265.09803805 0.00000000 00000-0 00000-0 0 01
2 29241 7.9177 51.8392 0007924 81.4875 278.6143 0.98859265 07
| Epoch (UTC): | 21 September 2020 02:21:10 |
| Eccentricity: | 0.0007924 |
| inclination: | 7.9177° |
| perigee height: | 36153 km |
| apogee height: | 36220 km |
| right ascension of ascending node: | 51.8392° |
| argument of perigee: | 81.4875° |
| revolutions per day: | 0.98859265 |
| mean anomaly at epoch: | 278.6143° |
| 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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