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 67190U 26145.59099375 +.00000000 +00000-0 +32487-3 0 00008
2 67190 43.0004 236.6343 0001317 273.1066 86.9635 15.27586774 09
| Epoch (UTC): | 25 May 2026 14:11:01 |
| Eccentricity: | 0.0001317 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.6343° |
| argument of perigee: | 273.1066° |
| revolutions per day: | 15.27586774 |
| mean anomaly at epoch: | 86.9635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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