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 39010U 12065C 23154.32751710 .00003518 00000-0 60044-3 0 9992
2 39010 49.6576 192.5407 4642254 282.9412 30.7063 6.21098160234556
| Epoch (UTC): | 03 June 2023 07:51:37 |
| Eccentricity: | 0.4642254 |
| inclination: | 49.6576° |
| perigee height: | 320 km |
| apogee height: | 11927 km |
| right ascension of ascending node: | 192.5407° |
| argument of perigee: | 282.9412° |
| revolutions per day: | 6.21098160 |
| mean anomaly at epoch: | 30.7063° |
| orbit number at epoch: | 23455 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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