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 67818U 26145.48012703 +.00000000 +00000-0 +57560-3 0 00002
2 67818 97.2875 333.6382 0001861 70.2143 289.9301 15.33451268 01
| Epoch (UTC): | 25 May 2026 11:31:22 |
| Eccentricity: | 0.0001861 |
| inclination: | 97.2875° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.6382° |
| argument of perigee: | 70.2143° |
| revolutions per day: | 15.33451268 |
| mean anomaly at epoch: | 289.9301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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