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 23155.61245368 .00094282 00000-0 11397-2 0 9999
2 39134 64.8492 328.6479 0018123 257.3083 102.6038 15.60002034561022
| Epoch (UTC): | 04 June 2023 14:41:55 |
| Eccentricity: | 0.0018123 |
| inclination: | 64.8492° |
| perigee height: | 375 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 328.6479° |
| argument of perigee: | 257.3083° |
| revolutions per day: | 15.60002034 |
| mean anomaly at epoch: | 102.6038° |
| orbit number at epoch: | 56102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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