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 23028.86509081 .00018244 00000-0 32393-3 0 9994
2 25544 51.6433 298.6263 0004574 288.3324 187.2023 15.50253619380180
| Epoch (UTC): | 28 January 2023 20:45:43 |
| Eccentricity: | 0.0004574 |
| inclination: | 51.6433° |
| perigee height: | 413 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 298.6263° |
| argument of perigee: | 288.3324° |
| revolutions per day: | 15.50253619 |
| mean anomaly at epoch: | 187.2023° |
| orbit number at epoch: | 38018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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