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 26474U 00047B 23154.60317719 .00002782 00000-0 23491-3 0 9994
2 26474 67.9936 336.3811 0047599 88.0533 272.6061 14.98836804241025
| Epoch (UTC): | 03 June 2023 14:28:34 |
| Eccentricity: | 0.0047599 |
| inclination: | 67.9936° |
| perigee height: | 537 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 336.3811° |
| argument of perigee: | 88.0533° |
| revolutions per day: | 14.98836804 |
| mean anomaly at epoch: | 272.6061° |
| orbit number at epoch: | 24102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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