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 23158.98705853 .00031294 00000-0 78620-3 0 9991
2 39136 64.8691 19.3083 0026985 273.2150 86.5900 15.39479125560265
| Epoch (UTC): | 07 June 2023 23:41:21 |
| Eccentricity: | 0.0026985 |
| inclination: | 64.8691° |
| perigee height: | 429 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 19.3083° |
| argument of perigee: | 273.2150° |
| revolutions per day: | 15.39479125 |
| mean anomaly at epoch: | 86.5900° |
| orbit number at epoch: | 56026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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