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 68454U 26145.36556383 +.00000000 +00000-0 +34525-3 0 00009
2 68454 97.4557 104.1188 0006775 129.8303 230.3528 15.17454470 01
| Epoch (UTC): | 25 May 2026 08:46:24 |
| Eccentricity: | 0.0006775 |
| inclination: | 97.4557° |
| perigee height: | 509 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 104.1188° |
| argument of perigee: | 129.8303° |
| revolutions per day: | 15.17454470 |
| mean anomaly at epoch: | 230.3528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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