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 67683U 26145.01594193 +.00000000 +00000-0 +54507-3 0 00007
2 67683 51.6300 50.8353 0011915 116.1156 244.1064 15.57682767 04
| Epoch (UTC): | 25 May 2026 00:22:57 |
| Eccentricity: | 0.0011915 |
| inclination: | 51.6300° |
| perigee height: | 386 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 50.8353° |
| argument of perigee: | 116.1156° |
| revolutions per day: | 15.57682767 |
| mean anomaly at epoch: | 244.1064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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