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 57350U 26145.36370637 +.00000000 +00000-0 +78158-5 0 00000
2 57350 43.0016 168.8396 0001269 286.3197 73.7515 15.27577677 03
| Epoch (UTC): | 25 May 2026 08:43:44 |
| Eccentricity: | 0.0001269 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.8396° |
| argument of perigee: | 286.3197° |
| revolutions per day: | 15.27577677 |
| mean anomaly at epoch: | 73.7515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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