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 47311U 21002C 23087.96355022 .00034490 00000-0 10144-2 0 9995
2 47311 60.6839 5.9711 0030082 132.0966 228.2692 15.34459117121963
| Epoch (UTC): | 28 March 2023 23:07:30 |
| Eccentricity: | 0.0030082 |
| inclination: | 60.6839° |
| perigee height: | 442 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 5.9711° |
| argument of perigee: | 132.0966° |
| revolutions per day: | 15.34459117 |
| mean anomaly at epoch: | 228.2692° |
| orbit number at epoch: | 12196 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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