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 68566U 26145.61590829 +.00000000 +00000-0 +95981-3 0 00007
2 68566 53.1599 4.4629 0000955 135.1340 224.9740 15.34412402 00
| Epoch (UTC): | 25 May 2026 14:46:54 |
| Eccentricity: | 0.0000955 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 4.4629° |
| argument of perigee: | 135.1340° |
| revolutions per day: | 15.34412402 |
| mean anomaly at epoch: | 224.9740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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