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 41173U 26145.61596358 +.00000000 +00000-0 +31699-4 0 00002
2 41173 97.4565 150.9739 0012660 148.6194 211.5804 15.30717500 06
| Epoch (UTC): | 25 May 2026 14:46:59 |
| Eccentricity: | 0.0012660 |
| inclination: | 97.4565° |
| perigee height: | 465 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 150.9739° |
| argument of perigee: | 148.6194° |
| revolutions per day: | 15.30717500 |
| mean anomaly at epoch: | 211.5804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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