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 23335.84870878 .00255250 00000-0 24337-2 0 9998
2 39136 64.8566 140.7808 0018537 260.1816 99.7240 15.65527492588137
| Epoch (UTC): | 01 December 2023 20:22:08 |
| Eccentricity: | 0.0018537 |
| inclination: | 64.8566° |
| perigee height: | 359 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 140.7808° |
| argument of perigee: | 260.1816° |
| revolutions per day: | 15.65527492 |
| mean anomaly at epoch: | 99.7240° |
| orbit number at epoch: | 58813 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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