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 37931U 11068B 24358.04356507 .00000497 00000-0 20660-3 0 9998
2 37931 98.7172 4.9241 0022064 294.5145 129.4947 14.30766173683374
| Epoch (UTC): | 23 December 2024 01:02:44 |
| Eccentricity: | 0.0022064 |
| inclination: | 98.7172° |
| perigee height: | 773 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 4.9241° |
| argument of perigee: | 294.5145° |
| revolutions per day: | 14.30766173 |
| mean anomaly at epoch: | 129.4947° |
| orbit number at epoch: | 68337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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