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 28415U 04035C 24277.85560865 .00019873 00000-0 95403-3 0 9999
2 28415 97.4139 309.2195 0040686 8.2017 351.9873 15.18147879100431
| Epoch (UTC): | 03 October 2024 20:32:04 |
| Eccentricity: | 0.0040686 |
| inclination: | 97.4139° |
| perigee height: | 483 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 309.2195° |
| argument of perigee: | 8.2017° |
| revolutions per day: | 15.18147879 |
| mean anomaly at epoch: | 351.9873° |
| orbit number at epoch: | 10043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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