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 37169U 10048B 23150.49923836 .00012450 00000-0 30382-3 0 9995
2 37169 97.9964 356.3330 0005648 86.0724 274.1166 15.41016052704682
| Epoch (UTC): | 30 May 2023 11:58:54 |
| Eccentricity: | 0.0005648 |
| inclination: | 97.9964° |
| perigee height: | 439 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 356.3330° |
| argument of perigee: | 86.0724° |
| revolutions per day: | 15.41016052 |
| mean anomaly at epoch: | 274.1166° |
| orbit number at epoch: | 70468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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