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 62508U 26145.58468488 +.00000000 +00000-0 +56484-3 0 00003
2 62508 43.0018 214.5376 0001346 263.7759 96.2940 15.27587734 09
| Epoch (UTC): | 25 May 2026 14:01:56 |
| Eccentricity: | 0.0001346 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 214.5376° |
| argument of perigee: | 263.7759° |
| revolutions per day: | 15.27587734 |
| mean anomaly at epoch: | 96.2940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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