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 59617U 26145.55064044 +.00000000 +00000-0 +50561-4 0 00008
2 59617 43.0027 324.1731 0001122 275.0719 85.0005 15.27575059 08
| Epoch (UTC): | 25 May 2026 13:12:55 |
| Eccentricity: | 0.0001122 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.1731° |
| argument of perigee: | 275.0719° |
| revolutions per day: | 15.27575059 |
| mean anomaly at epoch: | 85.0005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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