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 25861U 99039B 24311.51248820 .00002822 00000-0 37350-3 0 9998
2 25861 98.0699 358.4485 0015986 43.0273 317.2185 14.80660679364591
Epoch (UTC): | 06 November 2024 12:17:58 |
Eccentricity: | 0.0015986 |
inclination: | 98.0699° |
perigee height: | 616 km |
apogee height: | 638 km |
right ascension of ascending node: | 358.4485° |
argument of perigee: | 43.0273° |
revolutions per day: | 14.80660679 |
mean anomaly at epoch: | 317.2185° |
orbit number at epoch: | 36459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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