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 26087.82778278 +.00000000 +00000-0 +37100-3 0 00002
2 41846 98.4211 177.3609 0307417 351.0616 8.5179 14.54322500 03
| Epoch (UTC): | 28 March 2026 19:52:00 |
| Eccentricity: | 0.0307417 |
| inclination: | 98.4211° |
| perigee height: | 494 km |
| apogee height: | 930 km |
| right ascension of ascending node: | 177.3609° |
| argument of perigee: | 351.0616° |
| revolutions per day: | 14.54322500 |
| mean anomaly at epoch: | 8.5179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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