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 61636U 26145.52928204 +.00000000 +00000-0 -18147-4 0 00001
2 61636 43.0001 84.3985 0001606 271.8452 88.2215 15.27575970 05
| Epoch (UTC): | 25 May 2026 12:42:09 |
| Eccentricity: | 0.0001606 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.3985° |
| argument of perigee: | 271.8452° |
| revolutions per day: | 15.27575970 |
| mean anomaly at epoch: | 88.2215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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