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 43223U 18021A 25243.04956938 0.00000000 00000-0 00000-0 0 09
2 43223 97.3498 2.2205 0004771 326.0847 33.9152 15.27651077 00
| Epoch (UTC): | 31 August 2025 01:11:22 |
| Eccentricity: | 0.0004771 |
| inclination: | 97.3498° |
| perigee height: | 479 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 2.2205° |
| argument of perigee: | 326.0847° |
| revolutions per day: | 15.27651077 |
| mean anomaly at epoch: | 33.9152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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