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 41923U 17003G 24260.76428420 .00000214 00000-0 69320-4 0 9998
2 41923 86.4030 355.2282 0001986 99.4066 260.7354 14.34213056401749
| Epoch (UTC): | 16 September 2024 18:20:34 |
| Eccentricity: | 0.0001986 |
| inclination: | 86.4030° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 355.2282° |
| argument of perigee: | 99.4066° |
| revolutions per day: | 14.34213056 |
| mean anomaly at epoch: | 260.7354° |
| orbit number at epoch: | 40174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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