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 25344.46165267 .00000971 00000-0 20114-3 0 9996
2 46 66.6894 22.6118 0188531 74.6026 287.5825 14.54465516429555
| Epoch (UTC): | 10 December 2025 11:04:46 |
| Eccentricity: | 0.0188531 |
| inclination: | 66.6894° |
| perigee height: | 577 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 22.6118° |
| argument of perigee: | 74.6026° |
| revolutions per day: | 14.54465516 |
| mean anomaly at epoch: | 287.5825° |
| orbit number at epoch: | 42955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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