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 23038.17031632 .00000897 00000-0 21971-3 0 9990
2 47 66.6650 94.8802 0231778 316.0411 42.2456 14.42592025274232
| Epoch (UTC): | 07 February 2023 04:05:15 |
| Eccentricity: | 0.0231778 |
| inclination: | 66.6650° |
| perigee height: | 585 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 94.8802° |
| argument of perigee: | 316.0411° |
| revolutions per day: | 14.42592025 |
| mean anomaly at epoch: | 42.2456° |
| orbit number at epoch: | 27423 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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