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 58438U 26144.86294730 +.00000000 +00000-0 +63112-3 0 00003
2 58438 42.9991 331.4719 0001454 270.9160 89.1525 15.27588452 08
| Epoch (UTC): | 24 May 2026 20:42:38 |
| Eccentricity: | 0.0001454 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.4719° |
| argument of perigee: | 270.9160° |
| revolutions per day: | 15.27588452 |
| mean anomaly at epoch: | 89.1525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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