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 60172U 24121Q 24227.86663228 0.00000000 00000-0 00000-0 0 07
2 60172 70.0000 274.8314 0002000 179.6239 180.3760 14.96720000 07
| Epoch (UTC): | 14 August 2024 20:47:57 |
| Eccentricity: | 0.0002000 |
| inclination: | 70.0000° |
| perigee height: | 575 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 274.8314° |
| argument of perigee: | 179.6239° |
| revolutions per day: | 14.96720000 |
| mean anomaly at epoch: | 180.3760° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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