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 41851U 26145.34384579 +.00000000 +00000-0 +12549-3 0 00007
2 41851 98.0723 356.4350 0015315 189.6838 170.4096 15.09545433 00
| Epoch (UTC): | 25 May 2026 08:15:08 |
| Eccentricity: | 0.0015315 |
| inclination: | 98.0723° |
| perigee height: | 527 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 356.4350° |
| argument of perigee: | 189.6838° |
| revolutions per day: | 15.09545433 |
| mean anomaly at epoch: | 170.4096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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