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 58000U 26145.60074269 +.00000000 +00000-0 +70074-4 0 00000
2 58000 43.0015 352.2950 0001106 289.1685 70.9046 15.27572450 05
| Epoch (UTC): | 25 May 2026 14:25:04 |
| Eccentricity: | 0.0001106 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.2950° |
| argument of perigee: | 289.1685° |
| revolutions per day: | 15.27572450 |
| mean anomaly at epoch: | 70.9046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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