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 62593U 26145.64171047 +.00000000 +00000-0 +16829-2 0 00004
2 62593 43.0004 22.6058 0001067 253.7379 106.3371 15.70906321 06
| Epoch (UTC): | 25 May 2026 15:24:03 |
| Eccentricity: | 0.0001067 |
| inclination: | 43.0004° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 22.6058° |
| argument of perigee: | 253.7379° |
| revolutions per day: | 15.70906321 |
| mean anomaly at epoch: | 106.3371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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