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 23031.19183383 .00012034 00000-0 21617-3 0 9995
2 25544 51.6437 287.0940 0004835 295.6186 214.0137 15.50303496380549
| Epoch (UTC): | 31 January 2023 04:36:14 |
| Eccentricity: | 0.0004835 |
| inclination: | 51.6437° |
| perigee height: | 412 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 287.0940° |
| argument of perigee: | 295.6186° |
| revolutions per day: | 15.50303496 |
| mean anomaly at epoch: | 214.0137° |
| orbit number at epoch: | 38054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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