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 27464U 02036A 24259.89764154 .00000025 00000-0 10611-3 0 9999
2 27464 82.4874 24.6745 0025120 214.9360 145.0073 12.44604495 8143
| Epoch (UTC): | 15 September 2024 21:32:36 |
| Eccentricity: | 0.0025120 |
| inclination: | 82.4874° |
| perigee height: | 1467 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 24.6745° |
| argument of perigee: | 214.9360° |
| revolutions per day: | 12.44604495 |
| mean anomaly at epoch: | 145.0073° |
| orbit number at epoch: | 814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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