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 44741U 26145.34499780 +.00000000 +00000-0 +44160-3 0 00003
2 44741 53.0423 173.4567 0003143 329.5470 30.5362 15.67560390 04
| Epoch (UTC): | 25 May 2026 08:16:47 |
| Eccentricity: | 0.0003143 |
| inclination: | 53.0423° |
| perigee height: | 364 km |
| apogee height: | 368 km |
| right ascension of ascending node: | 173.4567° |
| argument of perigee: | 329.5470° |
| revolutions per day: | 15.67560390 |
| mean anomaly at epoch: | 30.5362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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