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 61641U 26145.16042590 +.00000000 +00000-0 -10652-3 0 00004
2 61641 43.0017 82.4580 0000884 239.5878 120.4887 15.27601046 06
| Epoch (UTC): | 25 May 2026 03:51:00 |
| Eccentricity: | 0.0000884 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 82.4580° |
| argument of perigee: | 239.5878° |
| revolutions per day: | 15.27601046 |
| mean anomaly at epoch: | 120.4887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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