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 41903U 26145.53429181 +.00000000 +00000-0 +00000-0 0 00001
2 41903 0.0165 345.5642 0000851 102.3172 97.6438 1.00270331 04
| Epoch (UTC): | 25 May 2026 12:49:22 |
| Eccentricity: | 0.0000851 |
| inclination: | 0.0165° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 345.5642° |
| argument of perigee: | 102.3172° |
| revolutions per day: | 1.00270331 |
| mean anomaly at epoch: | 97.6438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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