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 67581U 26145.40732574 +.00000000 +00000-0 +40615-3 0 00009
2 67581 97.2849 205.7705 0000892 94.0368 266.0977 15.33447227 08
| Epoch (UTC): | 25 May 2026 09:46:32 |
| Eccentricity: | 0.0000892 |
| inclination: | 97.2849° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.7705° |
| argument of perigee: | 94.0368° |
| revolutions per day: | 15.33447227 |
| mean anomaly at epoch: | 266.0977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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