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 23039.05791565 .00017615 00000-0 31902-3 0 9993
2 25544 51.6432 248.1296 0008064 325.6084 183.4434 15.49695988381767
| Epoch (UTC): | 08 February 2023 01:23:23 |
| Eccentricity: | 0.0008064 |
| inclination: | 51.6432° |
| perigee height: | 412 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 248.1296° |
| argument of perigee: | 325.6084° |
| revolutions per day: | 15.49695988 |
| mean anomaly at epoch: | 183.4434° |
| orbit number at epoch: | 38176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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