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 59934U 26145.35927237 +.00000000 +00000-0 -15582-4 0 00005
2 59934 43.0015 256.3380 0001402 269.6287 90.4404 15.27576232 00
| Epoch (UTC): | 25 May 2026 08:37:21 |
| Eccentricity: | 0.0001402 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 256.3380° |
| argument of perigee: | 269.6287° |
| revolutions per day: | 15.27576232 |
| mean anomaly at epoch: | 90.4404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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