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 23037.69601222 .00011883 00000-0 21841-3 0 9993
2 25544 51.6426 254.8733 0008269 320.8811 145.3384 15.49640401381550
| Epoch (UTC): | 06 February 2023 16:42:15 |
| Eccentricity: | 0.0008269 |
| inclination: | 51.6426° |
| perigee height: | 412 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 254.8733° |
| argument of perigee: | 320.8811° |
| revolutions per day: | 15.49640401 |
| mean anomaly at epoch: | 145.3384° |
| orbit number at epoch: | 38155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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