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 61634U 26145.52543314 +.00000000 +00000-0 +20038-4 0 00005
2 61634 43.0036 84.3670 0000691 244.4537 115.6244 15.27577464 02
| Epoch (UTC): | 25 May 2026 12:36:37 |
| Eccentricity: | 0.0000691 |
| inclination: | 43.0036° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.3670° |
| argument of perigee: | 244.4537° |
| revolutions per day: | 15.27577464 |
| mean anomaly at epoch: | 115.6244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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