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 23031.89406853 .00012191 00000-0 21874-3 0 9991
2 25544 51.6433 283.6121 0004719 296.3673 175.1106 15.50320722380654
| Epoch (UTC): | 31 January 2023 21:27:27 |
| Eccentricity: | 0.0004719 |
| inclination: | 51.6433° |
| perigee height: | 412 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 283.6121° |
| argument of perigee: | 296.3673° |
| revolutions per day: | 15.50320722 |
| mean anomaly at epoch: | 175.1106° |
| orbit number at epoch: | 38065 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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