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 27939U 03042A 24279.88284206 .00007529 00000-0 12393-2 0 9994
2 27939 98.3051 77.9820 0012692 72.5471 67.9786 14.70783327124548
| Epoch (UTC): | 05 October 2024 21:11:17 |
| Eccentricity: | 0.0012692 |
| inclination: | 98.3051° |
| perigee height: | 649 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 77.9820° |
| argument of perigee: | 72.5471° |
| revolutions per day: | 14.70783327 |
| mean anomaly at epoch: | 67.9786° |
| orbit number at epoch: | 12454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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