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 39026U 12072A 22145.85797402 .00019577 00000-0 55090-3 0 9999
2 39026 97.2671 136.8499 0028909 237.6186 122.2260 15.36086674525514
| Epoch (UTC): | 25 May 2022 20:35:28 |
| Eccentricity: | 0.0028909 |
| inclination: | 97.2671° |
| perigee height: | 438 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 136.8499° |
| argument of perigee: | 237.6186° |
| revolutions per day: | 15.36086674 |
| mean anomaly at epoch: | 122.2260° |
| orbit number at epoch: | 52551 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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