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 39439U 13066Z 24258.87935870 .00031482 00000-0 21901-2 0 9995
2 39439 97.7180 221.9920 0039616 186.2461 173.8276 15.04772741584346
Epoch (UTC): | 14 September 2024 21:06:16 |
Eccentricity: | 0.0039616 |
inclination: | 97.7180° |
perigee height: | 525 km |
apogee height: | 579 km |
right ascension of ascending node: | 221.9920° |
argument of perigee: | 186.2461° |
revolutions per day: | 15.04772741 |
mean anomaly at epoch: | 173.8276° |
orbit number at epoch: | 58434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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