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 58733U 26145.49196176 +.00000000 +00000-0 +61259-4 0 00007
2 58733 42.9990 145.6684 0001236 269.6488 90.4222 15.27581355 01
| Epoch (UTC): | 25 May 2026 11:48:25 |
| Eccentricity: | 0.0001236 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 145.6684° |
| argument of perigee: | 269.6488° |
| revolutions per day: | 15.27581355 |
| mean anomaly at epoch: | 90.4222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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