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 43115U 18004E 25137.20304171 .04606220 23996-5 59053-3 0 9992
2 43115 97.1894 221.7544 0010900 254.1267 105.8829 16.35734082410069
| Epoch (UTC): | 17 May 2025 04:52:22 |
| Eccentricity: | 0.0010900 |
| inclination: | 97.1894° |
| perigee height: | 170 km |
| apogee height: | 184 km |
| right ascension of ascending node: | 221.7544° |
| argument of perigee: | 254.1267° |
| revolutions per day: | 16.35734082 |
| mean anomaly at epoch: | 105.8829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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