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 59933U 26145.32925992 +.00000000 +00000-0 +78185-4 0 00004
2 59933 43.0011 259.7203 0001574 264.5766 95.4906 15.27577110 00
| Epoch (UTC): | 25 May 2026 07:54:08 |
| Eccentricity: | 0.0001574 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.7203° |
| argument of perigee: | 264.5766° |
| revolutions per day: | 15.27577110 |
| mean anomaly at epoch: | 95.4906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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