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 59174U 26145.50003470 +.00000000 +00000-0 +21669-2 0 00002
2 59174 43.0027 346.3275 0002196 267.2545 146.6678 15.27563143 08
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0002196 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 346.3275° |
| argument of perigee: | 267.2545° |
| revolutions per day: | 15.27563143 |
| mean anomaly at epoch: | 146.6678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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