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 68553U 26145.31547980 +.00000000 +00000-0 +89636-3 0 00000
2 68553 53.1598 6.1526 0001334 56.0707 304.0422 15.34407493 01
| Epoch (UTC): | 25 May 2026 07:34:17 |
| Eccentricity: | 0.0001334 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 6.1526° |
| argument of perigee: | 56.0707° |
| revolutions per day: | 15.34407493 |
| mean anomaly at epoch: | 304.0422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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