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 00047U 60007C 23088.84682689 .00000766 00000-0 18974-3 0 9997
2 00047 66.6660 319.2353 0233424 279.9582 77.5251 14.42759069281105
| Epoch (UTC): | 29 March 2023 20:19:25 |
| Eccentricity: | 0.0233424 |
| inclination: | 66.6660° |
| perigee height: | 583 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 319.2353° |
| argument of perigee: | 279.9582° |
| revolutions per day: | 14.42759069 |
| mean anomaly at epoch: | 77.5251° |
| orbit number at epoch: | 28110 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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