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 26155.72665175 +.00000000 +00000-0 +76043-3 0 00007
2 41846 98.4219 245.8533 0307196 141.7045 220.6409 14.54759869 07
| Epoch (UTC): | 04 June 2026 17:26:22 |
| Eccentricity: | 0.0307196 |
| inclination: | 98.4219° |
| perigee height: | 492 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 245.8533° |
| argument of perigee: | 141.7045° |
| revolutions per day: | 14.54759869 |
| mean anomaly at epoch: | 220.6409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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