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 27609U 02058E 24257.46106654 .00002426 00000-0 33604-3 0 9994
2 27609 64.5571 155.0907 0023663 337.3040 22.7016 14.80107039172833
| Epoch (UTC): | 13 September 2024 11:03:56 |
| Eccentricity: | 0.0023663 |
| inclination: | 64.5571° |
| perigee height: | 612 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 155.0907° |
| argument of perigee: | 337.3040° |
| revolutions per day: | 14.80107039 |
| mean anomaly at epoch: | 22.7016° |
| orbit number at epoch: | 17283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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