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 23344.55172951 .00010228 00000-0 18492-3 0 9991
2 25544 51.6394 174.9779 0001350 22.4129 73.1463 15.50313898429140
| Epoch (UTC): | 10 December 2023 13:14:29 |
| Eccentricity: | 0.0001350 |
| inclination: | 51.6394° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 174.9779° |
| argument of perigee: | 22.4129° |
| revolutions per day: | 15.50313898 |
| mean anomaly at epoch: | 73.1463° |
| orbit number at epoch: | 42914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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