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 67578U 26145.43997439 +.00000000 +00000-0 +10198-2 0 00003
2 67578 97.2858 205.7275 0000445 112.9668 247.1622 15.33442513 03
| Epoch (UTC): | 25 May 2026 10:33:33 |
| Eccentricity: | 0.0000445 |
| inclination: | 97.2858° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.7275° |
| argument of perigee: | 112.9668° |
| revolutions per day: | 15.33442513 |
| mean anomaly at epoch: | 247.1622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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