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 26155.29522139 +.00000000 +00000-0 +10685-3 0 00008
2 41898 98.5361 155.1721 0020524 353.1095 6.9819 14.59939797 01
| Epoch (UTC): | 04 June 2026 07:05:07 |
| Eccentricity: | 0.0020524 |
| inclination: | 98.5361° |
| perigee height: | 679 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 155.1721° |
| argument of perigee: | 353.1095° |
| revolutions per day: | 14.59939797 |
| mean anomaly at epoch: | 6.9819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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