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 41898U 26110.19778353 +.00000000 +00000-0 +94474-4 0 00008
2 41898 98.5370 108.7451 0021511 125.9730 234.3468 14.59901458 03
| Epoch (UTC): | 20 April 2026 04:44:48 |
| Eccentricity: | 0.0021511 |
| inclination: | 98.5370° |
| perigee height: | 678 km |
| apogee height: | 709 km |
| right ascension of ascending node: | 108.7451° |
| argument of perigee: | 125.9730° |
| revolutions per day: | 14.59901458 |
| mean anomaly at epoch: | 234.3468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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