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 61062U 26145.12957231 +.00000000 +00000-0 +12159-4 0 00008
2 61062 53.1597 294.5149 0001035 82.8199 277.2937 15.69710804 05
| Epoch (UTC): | 25 May 2026 03:06:35 |
| Eccentricity: | 0.0001035 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 294.5149° |
| argument of perigee: | 82.8199° |
| revolutions per day: | 15.69710804 |
| mean anomaly at epoch: | 277.2937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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