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 67957U 26145.28027749 +.00000000 +00000-0 +39800-3 0 00007
2 67957 43.0038 118.2297 0001233 279.7131 80.3581 15.27595120 05
| Epoch (UTC): | 25 May 2026 06:43:35 |
| Eccentricity: | 0.0001233 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.2297° |
| argument of perigee: | 279.7131° |
| revolutions per day: | 15.27595120 |
| mean anomaly at epoch: | 80.3581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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