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 17974U 87041B 24281.81472080 .00000407 00000-0 22367-3 0 9999
2 17974 71.0097 44.5747 0016240 275.4562 194.4445 14.17503055934939
| Epoch (UTC): | 07 October 2024 19:33:11 |
| Eccentricity: | 0.0016240 |
| inclination: | 71.0097° |
| perigee height: | 822 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 44.5747° |
| argument of perigee: | 275.4562° |
| revolutions per day: | 14.17503055 |
| mean anomaly at epoch: | 194.4445° |
| orbit number at epoch: | 93493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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