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 61862U 26145.03976169 +.00000000 +00000-0 +25191-4 0 00007
2 61862 43.0016 166.8701 0001465 291.7662 68.3034 15.27574673 08
| Epoch (UTC): | 25 May 2026 00:57:15 |
| Eccentricity: | 0.0001465 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 166.8701° |
| argument of perigee: | 291.7662° |
| revolutions per day: | 15.27574673 |
| mean anomaly at epoch: | 68.3034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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