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 61643U 26145.23352676 +.00000000 +00000-0 +38465-4 0 00005
2 61643 43.0032 82.1471 0001129 271.6990 88.3733 15.27581641 06
| Epoch (UTC): | 25 May 2026 05:36:16 |
| Eccentricity: | 0.0001129 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 82.1471° |
| argument of perigee: | 271.6990° |
| revolutions per day: | 15.27581641 |
| mean anomaly at epoch: | 88.3733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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