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 41770U 26145.59828983 +.00000000 +00000-0 +13833-3 0 00003
2 41770 98.2021 219.5359 0001425 83.3594 276.7767 14.58541769 03
| Epoch (UTC): | 25 May 2026 14:21:32 |
| Eccentricity: | 0.0001425 |
| inclination: | 98.2021° |
| perigee height: | 697 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 219.5359° |
| argument of perigee: | 83.3594° |
| revolutions per day: | 14.58541769 |
| mean anomaly at epoch: | 276.7767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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