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 67810U 26145.24085844 +.00000000 +00000-0 +64143-3 0 00009
2 67810 97.2859 333.3541 0001799 93.7654 266.3795 15.33445867 00
| Epoch (UTC): | 25 May 2026 05:46:50 |
| Eccentricity: | 0.0001799 |
| inclination: | 97.2859° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.3541° |
| argument of perigee: | 93.7654° |
| revolutions per day: | 15.33445867 |
| mean anomaly at epoch: | 266.3795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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