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 67080U 26145.40956954 +.00000000 +00000-0 +26600-3 0 00001
2 67080 70.0013 180.8442 0003169 270.7065 89.3730 14.98329047 04
| Epoch (UTC): | 25 May 2026 09:49:46 |
| Eccentricity: | 0.0003169 |
| inclination: | 70.0013° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 180.8442° |
| argument of perigee: | 270.7065° |
| revolutions per day: | 14.98329047 |
| mean anomaly at epoch: | 89.3730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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