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 54074C 22136Z 24281.14215278 .00030072 00000+0 18848-2 0 2817
2 54074 53.2141 151.5855 0001416 83.3124 13.5880 15.08826077 11
| Epoch (UTC): | 07 October 2024 03:24:42 |
| Eccentricity: | 0.0001416 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 151.5855° |
| argument of perigee: | 83.3124° |
| revolutions per day: | 15.08826077 |
| mean anomaly at epoch: | 13.5880° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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