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 43678U 18084H 24259.19465842 .00005732 00000-0 51622-3 0 9996
2 43678 98.0817 59.9123 0010203 94.0485 266.1901 14.95976039320371
| Epoch (UTC): | 15 September 2024 04:40:18 |
| Eccentricity: | 0.0010203 |
| inclination: | 98.0817° |
| perigee height: | 572 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 59.9123° |
| argument of perigee: | 94.0485° |
| revolutions per day: | 14.95976039 |
| mean anomaly at epoch: | 266.1901° |
| orbit number at epoch: | 32037 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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