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 29240U 06024A 20325.96379736 0.00000000 00000-0 00000-0 0 04
2 29240 3.3971 78.9809 0011182 212.0649 147.8793 0.98608484 06
| Epoch (UTC): | 20 November 2020 23:07:52 |
| Eccentricity: | 0.0011182 |
| inclination: | 3.3971° |
| perigee height: | 36211 km |
| apogee height: | 36307 km |
| right ascension of ascending node: | 78.9809° |
| argument of perigee: | 212.0649° |
| revolutions per day: | 0.98608484 |
| mean anomaly at epoch: | 147.8793° |
| 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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