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 59607U 26145.55915081 +.00000000 +00000-0 +58493-5 0 00006
2 59607 43.0040 327.6996 0001243 272.7417 87.3292 15.27574697 06
| Epoch (UTC): | 25 May 2026 13:25:10 |
| Eccentricity: | 0.0001243 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.6996° |
| argument of perigee: | 272.7417° |
| revolutions per day: | 15.27574697 |
| mean anomaly at epoch: | 87.3292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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