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 59693U 26145.54618609 +.00000000 +00000-0 +41539-4 0 00008
2 59693 43.0011 338.3016 0001086 272.7004 87.3723 15.27579136 00
| Epoch (UTC): | 25 May 2026 13:06:30 |
| Eccentricity: | 0.0001086 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.3016° |
| argument of perigee: | 272.7004° |
| revolutions per day: | 15.27579136 |
| mean anomaly at epoch: | 87.3723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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