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 26145.60677850 +.00000000 +00000-0 +96915-4 0 00008
2 41603 97.1486 142.4982 0012253 95.8370 264.4270 15.32940071 03
| Epoch (UTC): | 25 May 2026 14:33:45 |
| Eccentricity: | 0.0012253 |
| inclination: | 97.1486° |
| perigee height: | 459 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 142.4982° |
| argument of perigee: | 95.8370° |
| revolutions per day: | 15.32940071 |
| mean anomaly at epoch: | 264.4270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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