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 41901U 26145.43608568 +.00000000 +00000-0 +12597-3 0 00003
2 41901 98.5483 134.5350 0026110 36.9761 323.3231 14.59134633 03
| Epoch (UTC): | 25 May 2026 10:27:57 |
| Eccentricity: | 0.0026110 |
| inclination: | 98.5483° |
| perigee height: | 677 km |
| apogee height: | 714 km |
| right ascension of ascending node: | 134.5350° |
| argument of perigee: | 36.9761° |
| revolutions per day: | 14.59134633 |
| mean anomaly at epoch: | 323.3231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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