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 67218U 26145.25303855 +.00000000 +00000-0 +12672-3 0 00007
2 67218 70.0014 341.3870 0002583 266.6197 93.4666 14.98334344 06
| Epoch (UTC): | 25 May 2026 06:04:22 |
| Eccentricity: | 0.0002583 |
| inclination: | 70.0014° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.3870° |
| argument of perigee: | 266.6197° |
| revolutions per day: | 14.98334344 |
| mean anomaly at epoch: | 93.4666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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