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 67170U 26145.52946596 +.00000000 +00000-0 +70460-3 0 00008
2 67170 43.0002 237.0405 0001564 273.2171 86.8502 15.27596048 08
| Epoch (UTC): | 25 May 2026 12:42:25 |
| Eccentricity: | 0.0001564 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.0405° |
| argument of perigee: | 273.2171° |
| revolutions per day: | 15.27596048 |
| mean anomaly at epoch: | 86.8502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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