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 68443U 26145.36520696 +.00000000 +00000-0 +24179-3 0 00009
2 68443 97.4531 104.0992 0005820 134.1617 226.0096 15.17370736 04
| Epoch (UTC): | 25 May 2026 08:45:53 |
| Eccentricity: | 0.0005820 |
| inclination: | 97.4531° |
| perigee height: | 510 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 104.0992° |
| argument of perigee: | 134.1617° |
| revolutions per day: | 15.17370736 |
| mean anomaly at epoch: | 226.0096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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