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 62438U 26145.52223112 +.00000000 +00000-0 +55637-3 0 00001
2 62438 53.1614 338.2928 0001341 69.5462 290.5683 15.30240134 07
| Epoch (UTC): | 25 May 2026 12:32:00 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.2928° |
| argument of perigee: | 69.5462° |
| revolutions per day: | 15.30240134 |
| mean anomaly at epoch: | 290.5683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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