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 47U 60007C 23089.05479096 .00000786 00000-0 19401-3 0 9995
2 47 66.6660 318.6786 0233425 279.8112 77.6709 14.42759527281576
| Epoch (UTC): | 30 March 2023 01:18:53 |
| Eccentricity: | 0.0233425 |
| inclination: | 66.6660° |
| perigee height: | 583 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 318.6786° |
| argument of perigee: | 279.8112° |
| revolutions per day: | 14.42759527 |
| mean anomaly at epoch: | 77.6709° |
| orbit number at epoch: | 28157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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