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 65439U 26145.54755600 +.00000000 +00000-0 +21899-3 0 00002
2 65439 97.4475 359.7774 0001537 89.8438 270.2965 15.05655997 06
| Epoch (UTC): | 25 May 2026 13:08:28 |
| Eccentricity: | 0.0001537 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.7774° |
| argument of perigee: | 89.8438° |
| revolutions per day: | 15.05655997 |
| mean anomaly at epoch: | 270.2965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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