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 26099.19098615 +.00000000 +00000-0 +10908-3 0 00003
2 41603 97.1498 97.6310 0008373 261.3539 98.6755 15.32658652 03
| Epoch (UTC): | 09 April 2026 04:35:01 |
| Eccentricity: | 0.0008373 |
| inclination: | 97.1498° |
| perigee height: | 462 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 97.6310° |
| argument of perigee: | 261.3539° |
| revolutions per day: | 15.32658652 |
| mean anomaly at epoch: | 98.6755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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