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 39134U 13015E 22135.51296605 .00019288 00000-0 70712-3 0 9995
2 39134 64.8605 169.9296 0034305 286.9731 72.7641 15.27504929502204
| Epoch (UTC): | 15 May 2022 12:18:40 |
| Eccentricity: | 0.0034305 |
| inclination: | 64.8605° |
| perigee height: | 460 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 169.9296° |
| argument of perigee: | 286.9731° |
| revolutions per day: | 15.27504929 |
| mean anomaly at epoch: | 72.7641° |
| orbit number at epoch: | 50220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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