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 62230U 26145.26431104 +.00000000 +00000-0 +10143-2 0 00006
2 62230 53.1569 84.1283 0001491 41.4507 318.6623 15.69733630 08
| Epoch (UTC): | 25 May 2026 06:20:36 |
| Eccentricity: | 0.0001491 |
| inclination: | 53.1569° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 84.1283° |
| argument of perigee: | 41.4507° |
| revolutions per day: | 15.69733630 |
| mean anomaly at epoch: | 318.6623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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