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 67932U 26145.63548084 +.00000000 +00000-0 +88734-3 0 00009
2 67932 43.0002 116.5970 0001166 254.0084 106.0639 15.27586251 01
| Epoch (UTC): | 25 May 2026 15:15:05 |
| Eccentricity: | 0.0001166 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 116.5970° |
| argument of perigee: | 254.0084° |
| revolutions per day: | 15.27586251 |
| mean anomaly at epoch: | 106.0639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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