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 68809U 26145.56047206 +.00000000 +00000-0 +17988-2 0 00007
2 68809 97.2847 352.2263 0001260 122.9363 237.2024 15.75324071 03
| Epoch (UTC): | 25 May 2026 13:27:04 |
| Eccentricity: | 0.0001260 |
| inclination: | 97.2847° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2263° |
| argument of perigee: | 122.9363° |
| revolutions per day: | 15.75324071 |
| mean anomaly at epoch: | 237.2024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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