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 25137.58927511 .00000106 00000-0 13426-3 0 9992
2 5 34.2435 95.3223 1840975 154.8551 215.4388 10.85922780400361
| Epoch (UTC): | 17 May 2025 14:08:33 |
| Eccentricity: | 0.1840975 |
| inclination: | 34.2435° |
| perigee height: | 650 km |
| apogee height: | 3821 km |
| right ascension of ascending node: | 95.3223° |
| argument of perigee: | 154.8551° |
| revolutions per day: | 10.85922780 |
| mean anomaly at epoch: | 215.4388° |
| orbit number at epoch: | 40036 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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