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 65059U 26145.52975144 +.00000000 +00000-0 +24533-3 0 00003
2 65059 97.4460 222.6066 0002069 143.6283 216.5086 15.05657676 01
| Epoch (UTC): | 25 May 2026 12:42:50 |
| Eccentricity: | 0.0002069 |
| inclination: | 97.4460° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.6066° |
| argument of perigee: | 143.6283° |
| revolutions per day: | 15.05657676 |
| mean anomaly at epoch: | 216.5086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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