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 67640U 26145.50324527 +.00000000 +00000-0 +19374-3 0 00009
2 67640 43.0060 65.7687 0000929 354.1485 5.9356 15.27598544 05
| Epoch (UTC): | 25 May 2026 12:04:40 |
| Eccentricity: | 0.0000929 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 65.7687° |
| argument of perigee: | 354.1485° |
| revolutions per day: | 15.27598544 |
| mean anomaly at epoch: | 5.9356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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