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 23265.27748655 .00003782 00000-0 46718-3 0 9993
2 39151 98.0158 15.6857 0015728 191.9241 168.1602 14.83340958562073
| Epoch (UTC): | 22 September 2023 06:39:34 |
| Eccentricity: | 0.0015728 |
| inclination: | 98.0158° |
| perigee height: | 608 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 15.6857° |
| argument of perigee: | 191.9241° |
| revolutions per day: | 14.83340958 |
| mean anomaly at epoch: | 168.1602° |
| orbit number at epoch: | 56207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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