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 65063U 26145.57959944 +.00000000 +00000-0 +30622-3 0 00009
2 65063 97.4464 222.6972 0002257 132.9828 227.1589 15.05650396 09
| Epoch (UTC): | 25 May 2026 13:54:37 |
| Eccentricity: | 0.0002257 |
| inclination: | 97.4464° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.6972° |
| argument of perigee: | 132.9828° |
| revolutions per day: | 15.05650396 |
| mean anomaly at epoch: | 227.1589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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