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 59889U 26145.42995190 +.00000000 +00000-0 +19144-4 0 00002
2 59889 43.0022 48.5266 0001439 281.3237 78.7453 15.27583955 00
| Epoch (UTC): | 25 May 2026 10:19:07 |
| Eccentricity: | 0.0001439 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.5266° |
| argument of perigee: | 281.3237° |
| revolutions per day: | 15.27583955 |
| mean anomaly at epoch: | 78.7453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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