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 67943U 26145.40207832 +.00000000 +00000-0 +99500-3 0 00002
2 67943 42.9998 117.4213 0001363 263.8216 96.2481 15.27592598 05
| Epoch (UTC): | 25 May 2026 09:38:59 |
| Eccentricity: | 0.0001363 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 117.4213° |
| argument of perigee: | 263.8216° |
| revolutions per day: | 15.27592598 |
| mean anomaly at epoch: | 96.2481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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