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 06180U 72069B 24280.80738437 .00009421 00000-0 15190-2 0 9999
2 06180 90.0356 216.4678 0036492 174.4963 185.6664 14.70956320736629
| Epoch (UTC): | 06 October 2024 19:22:38 |
| Eccentricity: | 0.0036492 |
| inclination: | 90.0356° |
| perigee height: | 632 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 216.4678° |
| argument of perigee: | 174.4963° |
| revolutions per day: | 14.70956320 |
| mean anomaly at epoch: | 185.6664° |
| orbit number at epoch: | 73662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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