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 39467U 26145.44911735 +.00000000 +00000-0 +28248-3 0 00001
2 39467 120.4598 213.8613 0159974 332.4274 26.8384 15.08472113 07
| Epoch (UTC): | 25 May 2026 10:46:43 |
| Eccentricity: | 0.0159974 |
| inclination: | 120.4598° |
| perigee height: | 430 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 213.8613° |
| argument of perigee: | 332.4274° |
| revolutions per day: | 15.08472113 |
| mean anomaly at epoch: | 26.8384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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