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 67960U 26145.32767231 +.00000000 +00000-0 +35953-3 0 00008
2 67960 43.0021 117.7193 0001376 269.9318 90.1376 15.27592214 08
| Epoch (UTC): | 25 May 2026 07:51:50 |
| Eccentricity: | 0.0001376 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 117.7193° |
| argument of perigee: | 269.9318° |
| revolutions per day: | 15.27592214 |
| mean anomaly at epoch: | 90.1376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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