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 4607U 70025K 24357.99401477 .00000208 00000-0 10757-2 0 9995
2 4607 100.1634 348.4465 0613655 161.5678 273.6116 12.30977993455110
| Epoch (UTC): | 22 December 2024 23:51:22 |
| Eccentricity: | 0.0613655 |
| inclination: | 100.1634° |
| perigee height: | 1059 km |
| apogee height: | 2031 km |
| right ascension of ascending node: | 348.4465° |
| argument of perigee: | 161.5678° |
| revolutions per day: | 12.30977993 |
| mean anomaly at epoch: | 273.6116° |
| orbit number at epoch: | 45511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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