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 59241U 26145.07083391 +.00000000 +00000-0 +59520-4 0 00008
2 59241 43.0024 72.4842 0001057 240.8369 119.2377 15.27583052 06
| Epoch (UTC): | 25 May 2026 01:42:00 |
| Eccentricity: | 0.0001057 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 72.4842° |
| argument of perigee: | 240.8369° |
| revolutions per day: | 15.27583052 |
| mean anomaly at epoch: | 119.2377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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