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 67298U 26145.45687959 +.00000000 +00000-0 +28964-2 0 00007
2 67298 97.3882 222.3987 0005902 92.0828 268.1095 15.42901664 08
| Epoch (UTC): | 25 May 2026 10:57:54 |
| Eccentricity: | 0.0005902 |
| inclination: | 97.3882° |
| perigee height: | 434 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 222.3987° |
| argument of perigee: | 92.0828° |
| revolutions per day: | 15.42901664 |
| mean anomaly at epoch: | 268.1095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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