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 42830U 17042F 24253.13984836 .00107626 00000-0 37282-2 0 9995
2 42830 97.3710 88.7610 0006552 67.9083 292.2852 15.29382759390864
Epoch (UTC): | 09 September 2024 03:21:22 |
Eccentricity: | 0.0006552 |
inclination: | 97.3710° |
perigee height: | 473 km |
apogee height: | 482 km |
right ascension of ascending node: | 88.7610° |
argument of perigee: | 67.9083° |
revolutions per day: | 15.29382759 |
mean anomaly at epoch: | 292.2852° |
orbit number at epoch: | 39086 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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