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 41915U 17002C 21020.43029390 .00000544 00000-0 35381-4 0 9992
2 41915 97.3690 82.1588 0008567 254.3206 116.5091 15.11938726222345
| Epoch (UTC): | 20 January 2021 10:19:37 |
| Eccentricity: | 0.0008567 |
| inclination: | 97.3690° |
| perigee height: | 524 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 82.1588° |
| argument of perigee: | 254.3206° |
| revolutions per day: | 15.11938726 |
| mean anomaly at epoch: | 116.5091° |
| orbit number at epoch: | 22234 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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