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 39136U 13015G 23150.93052534 .00028462 00000-0 72799-3 0 9993
2 39136 64.8700 46.1763 0026583 274.7271 85.0830 15.38979547559023
| Epoch (UTC): | 30 May 2023 22:19:57 |
| Eccentricity: | 0.0026583 |
| inclination: | 64.8700° |
| perigee height: | 431 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 46.1763° |
| argument of perigee: | 274.7271° |
| revolutions per day: | 15.38979547 |
| mean anomaly at epoch: | 85.0830° |
| orbit number at epoch: | 55902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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