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 37954U 11075A 22258.91137150 0.00000000 00000-0 00000-0 0 01
2 37954 97.4860 333.9167 0002691 314.4319 45.5680 15.17620316 09
| Epoch (UTC): | 15 September 2022 21:52:22 |
| Eccentricity: | 0.0002691 |
| inclination: | 97.4860° |
| perigee height: | 511 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 333.9167° |
| argument of perigee: | 314.4319° |
| revolutions per day: | 15.17620316 |
| mean anomaly at epoch: | 45.5680° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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