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 23028.03913194 .00021754 00000-0 38481-3 0 9991
2 25544 51.6443 302.7162 0004959 283.9554 258.9968 15.50234023380057
| Epoch (UTC): | 28 January 2023 00:56:21 |
| Eccentricity: | 0.0004959 |
| inclination: | 51.6443° |
| perigee height: | 412 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 302.7162° |
| argument of perigee: | 283.9554° |
| revolutions per day: | 15.50234023 |
| mean anomaly at epoch: | 258.9968° |
| orbit number at epoch: | 38005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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