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 67093U 26145.48884375 +.00000000 +00000-0 +16054-3 0 00002
2 67093 70.0008 180.7210 0003851 267.2836 92.7882 14.98333740 00
| Epoch (UTC): | 25 May 2026 11:43:56 |
| Eccentricity: | 0.0003851 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.7210° |
| argument of perigee: | 267.2836° |
| revolutions per day: | 14.98333740 |
| mean anomaly at epoch: | 92.7882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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