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 23150.93288726 .00002547 00000-0 21602-3 0 9992
2 26474 67.9942 346.5301 0047639 92.5260 268.1339 14.98814638240478
| Epoch (UTC): | 30 May 2023 22:23:21 |
| Eccentricity: | 0.0047639 |
| inclination: | 67.9942° |
| perigee height: | 537 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 346.5301° |
| argument of perigee: | 92.5260° |
| revolutions per day: | 14.98814638 |
| mean anomaly at epoch: | 268.1339° |
| orbit number at epoch: | 24047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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