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 67812U 26145.58335647 +.00000000 +00000-0 -69776-3 0 00005
2 67812 97.2850 333.7266 0001390 83.3359 96.2870 15.33450739 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001390 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 333.7266° |
| argument of perigee: | 83.3359° |
| revolutions per day: | 15.33450739 |
| mean anomaly at epoch: | 96.2870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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