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 00059U 60013B 24261.94772492 .00000199 00000-0 14981-3 0 9998
2 00059 28.2472 157.7761 0188817 5.8688 354.4021 13.53090248156795
| Epoch (UTC): | 17 September 2024 22:44:43 |
| Eccentricity: | 0.0188817 |
| inclination: | 28.2472° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 157.7761° |
| argument of perigee: | 5.8688° |
| revolutions per day: | 13.53090248 |
| mean anomaly at epoch: | 354.4021° |
| orbit number at epoch: | 15679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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