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 59843U 26145.47107713 +.00000000 +00000-0 -61459-4 0 00000
2 59843 43.0019 200.3811 0001888 275.5641 84.4995 15.27560907 09
| Epoch (UTC): | 25 May 2026 11:18:21 |
| Eccentricity: | 0.0001888 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.3811° |
| argument of perigee: | 275.5641° |
| revolutions per day: | 15.27560907 |
| mean anomaly at epoch: | 84.4995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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