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 61858U 26145.42179950 +.00000000 +00000-0 -85329-4 0 00008
2 61858 43.0000 164.5762 0001275 276.8504 83.2203 15.27572651 04
| Epoch (UTC): | 25 May 2026 10:07:23 |
| Eccentricity: | 0.0001275 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5762° |
| argument of perigee: | 276.8504° |
| revolutions per day: | 15.27572651 |
| mean anomaly at epoch: | 83.2203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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