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 25318.67477412 .00002412 00000-0 46782-3 0 9999
2 46 66.6884 92.8555 0188488 94.8059 267.4602 14.54401545425805
| Epoch (UTC): | 14 November 2025 16:11:40 |
| Eccentricity: | 0.0188488 |
| inclination: | 66.6884° |
| perigee height: | 577 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 92.8555° |
| argument of perigee: | 94.8059° |
| revolutions per day: | 14.54401545 |
| mean anomaly at epoch: | 267.4602° |
| orbit number at epoch: | 42580 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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