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 62190U 26145.47158428 +.00000000 +00000-0 +29979-3 0 00007
2 62190 42.9790 141.1507 0000531 61.6454 298.4464 15.65183322 08
| Epoch (UTC): | 25 May 2026 11:19:04 |
| Eccentricity: | 0.0000531 |
| inclination: | 42.9790° |
| perigee height: | 372 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 141.1507° |
| argument of perigee: | 61.6454° |
| revolutions per day: | 15.65183322 |
| mean anomaly at epoch: | 298.4464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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