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 22178.31133609 .00010822 00000-0 38561-3 0 9995
2 39134 64.8626 29.5344 0034993 277.9973 81.7188 15.28753394508365
| Epoch (UTC): | 27 June 2022 07:28:19 |
| Eccentricity: | 0.0034993 |
| inclination: | 64.8626° |
| perigee height: | 455 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 29.5344° |
| argument of perigee: | 277.9973° |
| revolutions per day: | 15.28753394 |
| mean anomaly at epoch: | 81.7188° |
| orbit number at epoch: | 50836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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