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 37391U 11014B 24244.80576633 0.00000604 00000-0 83706-3 0 04
2 37391 63.4252 151.4590 0300499 356.8275 3.1247 13.40946767 07
| Epoch (UTC): | 31 August 2024 19:20:18 |
| Eccentricity: | 0.0300499 |
| inclination: | 63.4252° |
| perigee height: | 881 km |
| apogee height: | 1330 km |
| right ascension of ascending node: | 151.4590° |
| argument of perigee: | 356.8275° |
| revolutions per day: | 13.40946767 |
| mean anomaly at epoch: | 3.1247° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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