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 65068U 26145.48544236 +.00000000 +00000-0 +25945-3 0 00000
2 65068 97.4464 222.5154 0002034 145.4508 214.6852 15.05654196 08
| Epoch (UTC): | 25 May 2026 11:39:02 |
| Eccentricity: | 0.0002034 |
| inclination: | 97.4464° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.5154° |
| argument of perigee: | 145.4508° |
| revolutions per day: | 15.05654196 |
| mean anomaly at epoch: | 214.6852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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