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 41923U 26037.26048112 +.00000000 +00000-0 +14715-3 0 00005
2 41923 86.4021 143.1902 0002351 97.1181 263.0282 14.34222286 07
| Epoch (UTC): | 06 February 2026 06:15:05 |
| Eccentricity: | 0.0002351 |
| inclination: | 86.4021° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 143.1902° |
| argument of perigee: | 97.1181° |
| revolutions per day: | 14.34222286 |
| mean anomaly at epoch: | 263.0282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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