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 65061U 26145.23900581 +.00000000 +00000-0 +16184-3 0 00000
2 65061 97.4490 222.3871 0001371 162.9746 197.1528 15.05650742 03
| Epoch (UTC): | 25 May 2026 05:44:10 |
| Eccentricity: | 0.0001371 |
| inclination: | 97.4490° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 222.3871° |
| argument of perigee: | 162.9746° |
| revolutions per day: | 15.05650742 |
| mean anomaly at epoch: | 197.1528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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