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 37162U 10046A 22135.04077937 0.00000000 00000-0 00000-0 0 03
2 37162 123.0043 339.3092 0006249 1.9183 358.0003 13.41429550 09
| Epoch (UTC): | 15 May 2022 00:58:43 |
| Eccentricity: | 0.0006249 |
| inclination: | 123.0043° |
| perigee height: | 1099 km |
| apogee height: | 1108 km |
| right ascension of ascending node: | 339.3092° |
| argument of perigee: | 1.9183° |
| revolutions per day: | 13.41429550 |
| mean anomaly at epoch: | 358.0003° |
| 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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