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 68589U 26145.12560523 +.00000000 +00000-0 +78846-3 0 00007
2 68589 51.8756 288.3653 0006712 292.3178 67.7097 15.38326665 04
| Epoch (UTC): | 25 May 2026 03:00:52 |
| Eccentricity: | 0.0006712 |
| inclination: | 51.8756° |
| perigee height: | 446 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 288.3653° |
| argument of perigee: | 292.3178° |
| revolutions per day: | 15.38326665 |
| mean anomaly at epoch: | 67.7097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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