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 68016U 26145.38915998 +.00000000 +00000-0 +62490-3 0 00008
2 68016 97.2849 94.3446 0001828 105.0665 255.0780 15.33447517 01
| Epoch (UTC): | 25 May 2026 09:20:23 |
| Eccentricity: | 0.0001828 |
| inclination: | 97.2849° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3446° |
| argument of perigee: | 105.0665° |
| revolutions per day: | 15.33447517 |
| mean anomaly at epoch: | 255.0780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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