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 19650U 88102B 24283.89764008 .00000505 00000-0 27981-3 0 9991
2 19650 70.9992 156.6818 0012175 73.6858 286.5603 14.16022883853873
| Epoch (UTC): | 09 October 2024 21:32:36 |
| Eccentricity: | 0.0012175 |
| inclination: | 70.9992° |
| perigee height: | 830 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 156.6818° |
| argument of perigee: | 73.6858° |
| revolutions per day: | 14.16022883 |
| mean anomaly at epoch: | 286.5603° |
| orbit number at epoch: | 85387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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