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 26063.18004617 +.00000000 +00000-0 +15635-3 0 00000
2 41898 98.5347 60.3495 0019299 274.4447 85.4547 14.59864210 00
| Epoch (UTC): | 04 March 2026 04:19:15 |
| Eccentricity: | 0.0019299 |
| inclination: | 98.5347° |
| perigee height: | 680 km |
| apogee height: | 707 km |
| right ascension of ascending node: | 60.3495° |
| argument of perigee: | 274.4447° |
| revolutions per day: | 14.59864210 |
| mean anomaly at epoch: | 85.4547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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