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 67090U 26145.50570576 +.00000000 +00000-0 +95950-4 0 00000
2 67090 70.0015 180.7746 0003523 265.0353 95.0404 14.98338289 04
| Epoch (UTC): | 25 May 2026 12:08:12 |
| Eccentricity: | 0.0003523 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 180.7746° |
| argument of perigee: | 265.0353° |
| revolutions per day: | 14.98338289 |
| mean anomaly at epoch: | 95.0404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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