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 37673U 11024A 23159.54272324 .00001287 00000-0 20148-3 0 9999
2 37673 97.9995 168.4890 0002234 82.3042 31.5265 14.74414723644768
| Epoch (UTC): | 08 June 2023 13:01:31 |
| Eccentricity: | 0.0002234 |
| inclination: | 97.9995° |
| perigee height: | 645 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 168.4890° |
| argument of perigee: | 82.3042° |
| revolutions per day: | 14.74414723 |
| mean anomaly at epoch: | 31.5265° |
| orbit number at epoch: | 64476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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