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 23148.16410368 .00010137 00000-0 18391-3 0 9994
2 25544 51.6416 67.7932 0005332 29.4252 117.6511 15.50220421398684
| Epoch (UTC): | 28 May 2023 03:56:18 |
| Eccentricity: | 0.0005332 |
| inclination: | 51.6416° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 67.7932° |
| argument of perigee: | 29.4252° |
| revolutions per day: | 15.50220421 |
| mean anomaly at epoch: | 117.6511° |
| orbit number at epoch: | 39868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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