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 25134.00110015 .00001211 00000-0 23969-3 0 9993
2 46 66.6888 235.7132 0203403 234.5024 123.6963 14.53939979398930
| Epoch (UTC): | 14 May 2025 00:01:35 |
| Eccentricity: | 0.0203403 |
| inclination: | 66.6888° |
| perigee height: | 568 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 235.7132° |
| argument of perigee: | 234.5024° |
| revolutions per day: | 14.53939979 |
| mean anomaly at epoch: | 123.6963° |
| orbit number at epoch: | 39893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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