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 58734U 26145.49582087 +.00000000 +00000-0 +64822-4 0 00007
2 58734 42.9990 145.6961 0001358 266.2416 93.8280 15.27594350 09
| Epoch (UTC): | 25 May 2026 11:53:58 |
| Eccentricity: | 0.0001358 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 145.6961° |
| argument of perigee: | 266.2416° |
| revolutions per day: | 15.27594350 |
| mean anomaly at epoch: | 93.8280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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