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 68685U 26145.62715975 +.00000000 +00000-0 +13716-2 0 00006
2 68685 97.2863 18.3391 0001797 93.1329 267.0142 15.75261709 01
| Epoch (UTC): | 25 May 2026 15:03:06 |
| Eccentricity: | 0.0001797 |
| inclination: | 97.2863° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 18.3391° |
| argument of perigee: | 93.1329° |
| revolutions per day: | 15.75261709 |
| mean anomaly at epoch: | 267.0142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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