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 58748U 26145.46254705 +.00000000 +00000-0 -21502-3 0 00000
2 58748 43.0028 146.3118 0002160 272.8215 87.2390 15.27590909 07
| Epoch (UTC): | 25 May 2026 11:06:04 |
| Eccentricity: | 0.0002160 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.3118° |
| argument of perigee: | 272.8215° |
| revolutions per day: | 15.27590909 |
| mean anomaly at epoch: | 87.2390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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