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 26053.87458029 +.00000000 +00000-0 +14066-3 0 00006
2 41603 97.1477 53.8604 0012342 69.7334 290.5234 15.32232286 00
| Epoch (UTC): | 22 February 2026 20:59:23 |
| Eccentricity: | 0.0012342 |
| inclination: | 97.1477° |
| perigee height: | 461 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 53.8604° |
| argument of perigee: | 69.7334° |
| revolutions per day: | 15.32232286 |
| mean anomaly at epoch: | 290.5234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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