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 6155U 72065B 24282.19311373 .00015996 00000-0 22990-2 0 9997
2 6155 35.0016 93.7242 0035768 340.2251 19.7061 14.75260491785639
| Epoch (UTC): | 08 October 2024 04:38:05 |
| Eccentricity: | 0.0035768 |
| inclination: | 35.0016° |
| perigee height: | 619 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 93.7242° |
| argument of perigee: | 340.2251° |
| revolutions per day: | 14.75260491 |
| mean anomaly at epoch: | 19.7061° |
| orbit number at epoch: | 78563 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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