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 23276.41051990 .00021266 00000-0 38303-3 0 9996
2 25544 51.6417 152.4854 0005370 65.2174 107.7396 15.49734051418572
| Epoch (UTC): | 03 October 2023 09:51:08 |
| Eccentricity: | 0.0005370 |
| inclination: | 51.6417° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 152.4854° |
| argument of perigee: | 65.2174° |
| revolutions per day: | 15.49734051 |
| mean anomaly at epoch: | 107.7396° |
| orbit number at epoch: | 41857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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