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 22180.53550023 .00006223 00000-0 22510-3 0 9992
2 39134 64.8620 22.2315 0035146 277.5185 82.1954 15.28785506509085
| Epoch (UTC): | 29 June 2022 12:51:07 |
| Eccentricity: | 0.0035146 |
| inclination: | 64.8620° |
| perigee height: | 455 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 22.2315° |
| argument of perigee: | 277.5185° |
| revolutions per day: | 15.28785506 |
| mean anomaly at epoch: | 82.1954° |
| orbit number at epoch: | 50908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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