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 23037.88453675 .00012029 00000-0 22097-3 0 9998
2 25544 51.6427 253.9395 0008245 321.2765 117.3645 15.49645655381580
| Epoch (UTC): | 06 February 2023 21:13:43 |
| Eccentricity: | 0.0008245 |
| inclination: | 51.6427° |
| perigee height: | 412 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 253.9395° |
| argument of perigee: | 321.2765° |
| revolutions per day: | 15.49645655 |
| mean anomaly at epoch: | 117.3645° |
| orbit number at epoch: | 38158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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