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 5U 58002B 25139.88778395 .00000092 00000-0 11199-3 0 9990
2 5 34.2449 88.2258 1840985 165.2219 201.0528 10.85923107400612
Epoch (UTC): | 19 May 2025 21:18:24 |
Eccentricity: | 0.1840985 |
inclination: | 34.2449° |
perigee height: | 650 km |
apogee height: | 3821 km |
right ascension of ascending node: | 88.2258° |
argument of perigee: | 165.2219° |
revolutions per day: | 10.85923107 |
mean anomaly at epoch: | 201.0528° |
orbit number at epoch: | 40061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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