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 23151.93388081 .00002678 00000-0 22656-3 0 9993
2 26474 67.9940 343.7622 0047620 91.2952 269.3648 14.98820656240704
| Epoch (UTC): | 31 May 2023 22:24:47 |
| Eccentricity: | 0.0047620 |
| inclination: | 67.9940° |
| perigee height: | 537 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 343.7622° |
| argument of perigee: | 91.2952° |
| revolutions per day: | 14.98820656 |
| mean anomaly at epoch: | 269.3648° |
| orbit number at epoch: | 24070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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