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 is defined by the following mean orbital elements,
1 674U 63039A 25233.70687258 -.00000484 00000-0 00000+0 0 9992
2 674 46.9199 107.0652 5061239 83.4591 359.8149 0.22192263 50173
| Epoch (UTC): | 21 August 2025 16:57:53 |
| Eccentricity: | 0.5061239 |
| inclination: | 46.9199° |
| perigee height: | 50535 km |
| apogee height: | 167185 km |
| right ascension of ascending node: | 107.0652° |
| argument of perigee: | 83.4591° |
| revolutions per day: | 0.22192263 |
| mean anomaly at epoch: | 359.8149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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