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 37932U 11068C 24281.59636568 .00000856 00000-0 40014-3 0 9996
2 37932 98.8059 223.2309 0035779 238.5312 294.6628 14.22638938668655
| Epoch (UTC): | 07 October 2024 14:18:45 |
| Eccentricity: | 0.0035779 |
| inclination: | 98.8059° |
| perigee height: | 791 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 223.2309° |
| argument of perigee: | 238.5312° |
| revolutions per day: | 14.22638938 |
| mean anomaly at epoch: | 294.6628° |
| orbit number at epoch: | 66865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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