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 23091.97159431 .00097458 00000-0 17954-2 0 9995
2 39134 64.8541 185.8619 0018580 260.6646 99.2394 15.48430149551512
| Epoch (UTC): | 01 April 2023 23:19:05 |
| Eccentricity: | 0.0018580 |
| inclination: | 64.8541° |
| perigee height: | 408 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 185.8619° |
| argument of perigee: | 260.6646° |
| revolutions per day: | 15.48430149 |
| mean anomaly at epoch: | 99.2394° |
| orbit number at epoch: | 55151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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