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 68473U 26145.37797999 +.00000000 +00000-0 +68009-3 0 00005
2 68473 97.4535 104.2265 0008242 207.5517 152.5283 15.21267219 08
| Epoch (UTC): | 25 May 2026 09:04:17 |
| Eccentricity: | 0.0008242 |
| inclination: | 97.4535° |
| perigee height: | 496 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 104.2265° |
| argument of perigee: | 207.5517° |
| revolutions per day: | 15.21267219 |
| mean anomaly at epoch: | 152.5283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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