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 00005U 58002B 25340.58840661 .00000314 00000-0 40348-3 0 9992
2 00005 34.2445 188.7345 1840333 350.0710 6.7767 10.85933996422344
| Epoch (UTC): | 06 December 2025 14:07:18 |
| Eccentricity: | 0.1840333 |
| inclination: | 34.2445° |
| perigee height: | 650 km |
| apogee height: | 3821 km |
| right ascension of ascending node: | 188.7345° |
| argument of perigee: | 350.0710° |
| revolutions per day: | 10.85933996 |
| mean anomaly at epoch: | 6.7767° |
| orbit number at epoch: | 42234 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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