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 67196U 26145.48655294 +.00000000 +00000-0 +35892-3 0 00003
2 67196 70.0020 341.0092 0002802 265.1030 94.9809 14.98333335 09
| Epoch (UTC): | 25 May 2026 11:40:38 |
| Eccentricity: | 0.0002802 |
| inclination: | 70.0020° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 341.0092° |
| argument of perigee: | 265.1030° |
| revolutions per day: | 14.98333335 |
| mean anomaly at epoch: | 94.9809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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