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 23266.34540382 .00017378 00000-0 31652-3 0 9994
2 25544 51.6416 202.3244 0005870 51.2241 92.3610 15.49559831417011
| Epoch (UTC): | 23 September 2023 08:17:22 |
| Eccentricity: | 0.0005870 |
| inclination: | 51.6416° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 202.3244° |
| argument of perigee: | 51.2241° |
| revolutions per day: | 15.49559831 |
| mean anomaly at epoch: | 92.3610° |
| orbit number at epoch: | 41701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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