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 65058U 26145.46883230 +.00000000 +00000-0 +27083-3 0 00002
2 65058 97.4457 222.5359 0002862 142.2835 217.8594 15.05655702 05
| Epoch (UTC): | 25 May 2026 11:15:07 |
| Eccentricity: | 0.0002862 |
| inclination: | 97.4457° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.5359° |
| argument of perigee: | 142.2835° |
| revolutions per day: | 15.05655702 |
| mean anomaly at epoch: | 217.8594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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