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 29242U 06024C 21151.37290446 0.00000000 00000-0 00000-0 0 09
2 29242 9.6761 33.8220 0004388 113.8267 246.2314 1.04030032 04
| Epoch (UTC): | 31 May 2021 08:56:58 |
| Eccentricity: | 0.0004388 |
| inclination: | 9.6761° |
| perigee height: | 34746 km |
| apogee height: | 34782 km |
| right ascension of ascending node: | 33.8220° |
| argument of perigee: | 113.8267° |
| revolutions per day: | 1.04030032 |
| mean anomaly at epoch: | 246.2314° |
| 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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