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 41792U 16059K 24357.68916644 .00006439 00000-0 97416-3 0 9991
2 41792 97.8273 25.6164 0024451 104.5605 255.8319 14.74339280440925
Epoch (UTC): | 22 December 2024 16:32:23 |
Eccentricity: | 0.0024451 |
inclination: | 97.8273° |
perigee height: | 630 km |
apogee height: | 664 km |
right ascension of ascending node: | 25.6164° |
argument of perigee: | 104.5605° |
revolutions per day: | 14.74339280 |
mean anomaly at epoch: | 255.8319° |
orbit number at epoch: | 44092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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