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 27840U 03031A 24259.88851218 .00000701 00000-0 22643-3 0 9999
2 27840 98.5430 227.0224 0098691 90.4954 270.7543 14.39446355114014
| Epoch (UTC): | 15 September 2024 21:19:27 |
| Eccentricity: | 0.0098691 |
| inclination: | 98.5430° |
| perigee height: | 690 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 227.0224° |
| argument of perigee: | 90.4954° |
| revolutions per day: | 14.39446355 |
| mean anomaly at epoch: | 270.7543° |
| orbit number at epoch: | 11401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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