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 58448U 26145.55006811 +.00000000 +00000-0 +18648-4 0 00007
2 58448 43.0039 327.1241 0001202 270.6141 89.4573 15.27575300 07
| Epoch (UTC): | 25 May 2026 13:12:05 |
| Eccentricity: | 0.0001202 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.1241° |
| argument of perigee: | 270.6141° |
| revolutions per day: | 15.27575300 |
| mean anomaly at epoch: | 89.4573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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