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 59193U 26145.03872109 +.00000000 +00000-0 +38582-4 0 00008
2 59193 43.0037 21.7369 0000754 288.0617 72.0152 15.27573724 02
| Epoch (UTC): | 25 May 2026 00:55:45 |
| Eccentricity: | 0.0000754 |
| inclination: | 43.0037° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.7369° |
| argument of perigee: | 288.0617° |
| revolutions per day: | 15.27573724 |
| mean anomaly at epoch: | 72.0152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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