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 67075U 26145.38471596 +.00000000 +00000-0 +30280-3 0 00005
2 67075 70.0010 181.1575 0002962 273.2817 86.8003 14.98349300 08
| Epoch (UTC): | 25 May 2026 09:13:59 |
| Eccentricity: | 0.0002962 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 181.1575° |
| argument of perigee: | 273.2817° |
| revolutions per day: | 14.98349300 |
| mean anomaly at epoch: | 86.8003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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