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 25343.90093048 .00000219 00000-0 29097-3 0 9992
2 00005 34.2416 178.5066 1840124 5.0159 356.6413 10.85935456422709
| Epoch (UTC): | 09 December 2025 21:37:20 |
| Eccentricity: | 0.1840124 |
| inclination: | 34.2416° |
| perigee height: | 650 km |
| apogee height: | 3821 km |
| right ascension of ascending node: | 178.5066° |
| argument of perigee: | 5.0159° |
| revolutions per day: | 10.85935456 |
| mean anomaly at epoch: | 356.6413° |
| orbit number at epoch: | 42270 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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