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 38341U 12025E 22144.54970262 .00001713 00000-0 20428-3 0 9998
2 38341 98.5077 358.2288 0055802 122.8596 237.8006 14.84675364542102
| Epoch (UTC): | 24 May 2022 13:11:34 |
| Eccentricity: | 0.0055802 |
| inclination: | 98.5077° |
| perigee height: | 575 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 358.2288° |
| argument of perigee: | 122.8596° |
| revolutions per day: | 14.84675364 |
| mean anomaly at epoch: | 237.8006° |
| orbit number at epoch: | 54210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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