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 39151U 13018B 23088.81917061 .00004665 00000-0 58892-3 0 9992
2 39151 97.9995 198.9235 0017045 53.1863 307.0911 14.82301377535920
| Epoch (UTC): | 29 March 2023 19:39:36 |
| Eccentricity: | 0.0017045 |
| inclination: | 97.9995° |
| perigee height: | 610 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 198.9235° |
| argument of perigee: | 53.1863° |
| revolutions per day: | 14.82301377 |
| mean anomaly at epoch: | 307.0911° |
| orbit number at epoch: | 53592 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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