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 62523U 26145.63999537 +.00000000 +00000-0 +18037-2 0 00001
2 62523 42.9992 326.6433 0001553 272.7028 87.3662 15.70820334 09
| Epoch (UTC): | 25 May 2026 15:21:35 |
| Eccentricity: | 0.0001553 |
| inclination: | 42.9992° |
| perigee height: | 356 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 326.6433° |
| argument of perigee: | 272.7028° |
| revolutions per day: | 15.70820334 |
| mean anomaly at epoch: | 87.3662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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