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 59943U 26145.60493250 +.00000000 +00000-0 +21167-3 0 00000
2 59943 42.9990 258.3499 0001184 269.8400 90.2316 15.27580917 04
| Epoch (UTC): | 25 May 2026 14:31:06 |
| Eccentricity: | 0.0001184 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 258.3499° |
| argument of perigee: | 269.8400° |
| revolutions per day: | 15.27580917 |
| mean anomaly at epoch: | 90.2316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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