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 is defined by the following mean orbital elements,
1 37377U 11011A 24007.64408617 0.00000000 00000-0 00000-0 0 03
2 37377 5.1648 27.4689 0037960 112.5293 247.8852 0.99118484 07
| Epoch (UTC): | 07 January 2024 15:27:29 |
| Eccentricity: | 0.0037960 |
| inclination: | 5.1648° |
| perigee height: | 35951 km |
| apogee height: | 36274 km |
| right ascension of ascending node: | 27.4689° |
| argument of perigee: | 112.5293° |
| revolutions per day: | 0.99118484 |
| mean anomaly at epoch: | 247.8852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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