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 41603U 26150.89410498 +.00000000 +00000-0 +13820-3 0 00001
2 41603 97.1480 147.6101 0012199 80.0279 280.2340 15.32984793 03
| Epoch (UTC): | 30 May 2026 21:27:30 |
| Eccentricity: | 0.0012199 |
| inclination: | 97.1480° |
| perigee height: | 459 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 147.6101° |
| argument of perigee: | 80.0279° |
| revolutions per day: | 15.32984793 |
| mean anomaly at epoch: | 280.2340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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