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 38770U 12048N 23340.22859108 0.00017500 00000-0 91099-3 0 04
2 38770 64.6539 101.8081 0101627 97.5891 262.4109 15.11308035 06
| Epoch (UTC): | 06 December 2023 05:29:10 |
| Eccentricity: | 0.0101627 |
| inclination: | 64.6539° |
| perigee height: | 462 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 101.8081° |
| argument of perigee: | 97.5891° |
| revolutions per day: | 15.11308035 |
| mean anomaly at epoch: | 262.4109° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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