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 25544U 98067A 23337.52021014 .00021640 00000-0 38462-3 0 9992
2 25544 51.6419 209.8257 0000784 18.3680 49.4844 15.50109640428059
| Epoch (UTC): | 03 December 2023 12:29:06 |
| Eccentricity: | 0.0000784 |
| inclination: | 51.6419° |
| perigee height: | 416 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 209.8257° |
| argument of perigee: | 18.3680° |
| revolutions per day: | 15.50109640 |
| mean anomaly at epoch: | 49.4844° |
| orbit number at epoch: | 42805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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