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 23338.05416302 .00025143 00000-0 44481-3 0 9999
2 25544 51.6419 207.1799 0001187 14.3718 155.1850 15.50148145428131
| Epoch (UTC): | 04 December 2023 01:17:59 |
| Eccentricity: | 0.0001187 |
| inclination: | 51.6419° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 207.1799° |
| argument of perigee: | 14.3718° |
| revolutions per day: | 15.50148145 |
| mean anomaly at epoch: | 155.1850° |
| orbit number at epoch: | 42813 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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