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 28493U 04049B 23272.54511640 .00002149 00000-0 32489-3 0 9990
2 28493 98.1306 19.3898 0003417 220.7547 139.3406 14.75299778 9009
| Epoch (UTC): | 29 September 2023 13:04:58 |
| Eccentricity: | 0.0003417 |
| inclination: | 98.1306° |
| perigee height: | 642 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 19.3898° |
| argument of perigee: | 220.7547° |
| revolutions per day: | 14.75299778 |
| mean anomaly at epoch: | 139.3406° |
| orbit number at epoch: | 900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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