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 67946U 26145.31867282 +.00000000 +00000-0 +55620-3 0 00001
2 67946 43.0037 117.6400 0002074 289.8532 70.2096 15.27596840 01
| Epoch (UTC): | 25 May 2026 07:38:53 |
| Eccentricity: | 0.0002074 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 117.6400° |
| argument of perigee: | 289.8532° |
| revolutions per day: | 15.27596840 |
| mean anomaly at epoch: | 70.2096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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