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 41846U 26032.22886725 +.00000000 +00000-0 +72533-3 0 00002
2 41846 98.4283 121.3045 0310108 161.6801 199.5868 14.53817203 01
| Epoch (UTC): | 01 February 2026 05:29:34 |
| Eccentricity: | 0.0310108 |
| inclination: | 98.4283° |
| perigee height: | 493 km |
| apogee height: | 933 km |
| right ascension of ascending node: | 121.3045° |
| argument of perigee: | 161.6801° |
| revolutions per day: | 14.53817203 |
| mean anomaly at epoch: | 199.5868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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