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 46U 60007B 25338.54795855 .00001267 00000-0 25588-3 0 9999
2 46 66.6897 38.7218 0188398 79.2253 283.0002 14.54452606428699
| Epoch (UTC): | 04 December 2025 13:09:03 |
| Eccentricity: | 0.0188398 |
| inclination: | 66.6897° |
| perigee height: | 577 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 38.7218° |
| argument of perigee: | 79.2253° |
| revolutions per day: | 14.54452606 |
| mean anomaly at epoch: | 283.0002° |
| orbit number at epoch: | 42869 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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