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 42836U 17042M 21023.66584912 .00000331 00000-0 38428-4 0 9992
2 42836 97.4919 261.2219 0011709 272.6747 87.3132 14.91413897192148
| Epoch (UTC): | 23 January 2021 15:58:49 |
| Eccentricity: | 0.0011709 |
| inclination: | 97.4919° |
| perigee height: | 585 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 261.2219° |
| argument of perigee: | 272.6747° |
| revolutions per day: | 14.91413897 |
| mean anomaly at epoch: | 87.3132° |
| orbit number at epoch: | 19214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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