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 23338.68696926 .00002505 00000-0 51547-4 0 9999
2 25544 51.6407 204.0474 0001105 4.6157 98.7044 15.50161098428233
| Epoch (UTC): | 04 December 2023 16:29:14 |
| Eccentricity: | 0.0001105 |
| inclination: | 51.6407° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 204.0474° |
| argument of perigee: | 4.6157° |
| revolutions per day: | 15.50161098 |
| mean anomaly at epoch: | 98.7044° |
| orbit number at epoch: | 42823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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