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 59045U 26145.50632123 +.00000000 +00000-0 +29098-4 0 00008
2 59045 42.9993 309.9749 0000606 97.4304 262.6616 15.27575476 09
| Epoch (UTC): | 25 May 2026 12:09:06 |
| Eccentricity: | 0.0000606 |
| inclination: | 42.9993° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 309.9749° |
| argument of perigee: | 97.4304° |
| revolutions per day: | 15.27575476 |
| mean anomaly at epoch: | 262.6616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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