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 41465U 16026B 22181.17550973 .00008373 00000-0 19970-3 0 9996
2 41465 97.0541 57.0952 0011631 87.9110 27.9160 15.41727394345497
| Epoch (UTC): | 30 June 2022 04:12:44 |
| Eccentricity: | 0.0011631 |
| inclination: | 97.0541° |
| perigee height: | 433 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 57.0952° |
| argument of perigee: | 87.9110° |
| revolutions per day: | 15.41727394 |
| mean anomaly at epoch: | 27.9160° |
| orbit number at epoch: | 34549 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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