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 51744C 22016AG 24358.19076389 .00007949 00000+0 49832-3 0 3583
2 51744 53.2150 141.1145 0001331 85.0373 231.1008 15.08838301 13
| Epoch (UTC): | 23 December 2024 04:34:42 |
| Eccentricity: | 0.0001331 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 141.1145° |
| argument of perigee: | 85.0373° |
| revolutions per day: | 15.08838301 |
| mean anomaly at epoch: | 231.1008° |
| 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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