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 23038.32129630 .00014376 00000-0 26225-3 0 9993
2 25544 51.6429 251.7773 0008243 323.0854 33.7469 15.49662718381646
| Epoch (UTC): | 07 February 2023 07:42:40 |
| Eccentricity: | 0.0008243 |
| inclination: | 51.6429° |
| perigee height: | 412 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 251.7773° |
| argument of perigee: | 323.0854° |
| revolutions per day: | 15.49662718 |
| mean anomaly at epoch: | 33.7469° |
| orbit number at epoch: | 38164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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