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 62439U 26145.56233179 +.00000000 +00000-0 +40509-3 0 00002
2 62439 53.1607 338.5418 0001189 102.0856 258.0278 15.30206923 04
| Epoch (UTC): | 25 May 2026 13:29:45 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.5418° |
| argument of perigee: | 102.0856° |
| revolutions per day: | 15.30206923 |
| mean anomaly at epoch: | 258.0278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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