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 23081.50174717 .00092393 00000-0 18292-2 0 9996
2 39134 64.8542 221.2305 0019916 253.7866 106.1083 15.46347006549899
| Epoch (UTC): | 22 March 2023 12:02:30 |
| Eccentricity: | 0.0019916 |
| inclination: | 64.8542° |
| perigee height: | 414 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 221.2305° |
| argument of perigee: | 253.7866° |
| revolutions per day: | 15.46347006 |
| mean anomaly at epoch: | 106.1083° |
| orbit number at epoch: | 54989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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