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 59188U 26145.33353036 +.00000000 +00000-0 +15700-2 0 00003
2 59188 43.0004 19.6437 0002109 266.8374 93.2237 15.27637485 06
| Epoch (UTC): | 25 May 2026 08:00:17 |
| Eccentricity: | 0.0002109 |
| inclination: | 43.0004° |
| perigee height: | 481 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.6437° |
| argument of perigee: | 266.8374° |
| revolutions per day: | 15.27637485 |
| mean anomaly at epoch: | 93.2237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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