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 68892U 26144.99777844 +.00000000 +00000-0 +10733-2 0 00004
2 68892 51.8825 354.3759 0001680 196.0854 164.0080 15.38433266 08
| Epoch (UTC): | 24 May 2026 23:56:48 |
| Eccentricity: | 0.0001680 |
| inclination: | 51.8825° |
| perigee height: | 450 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 354.3759° |
| argument of perigee: | 196.0854° |
| revolutions per day: | 15.38433266 |
| mean anomaly at epoch: | 164.0080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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