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 23150.10963392 .00012160 00000-0 29691-3 0 9993
2 37169 97.9965 355.9068 0005662 87.1588 273.0304 15.41005760704644
| Epoch (UTC): | 30 May 2023 02:37:52 |
| Eccentricity: | 0.0005662 |
| inclination: | 97.9965° |
| perigee height: | 439 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 355.9068° |
| argument of perigee: | 87.1588° |
| revolutions per day: | 15.41005760 |
| mean anomaly at epoch: | 273.0304° |
| orbit number at epoch: | 70464 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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