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 68804U 26145.56506610 +.00000000 +00000-0 +14357-2 0 00008
2 68804 97.2854 352.2202 0001228 90.5357 269.6049 15.75261819 02
| Epoch (UTC): | 25 May 2026 13:33:41 |
| Eccentricity: | 0.0001228 |
| inclination: | 97.2854° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2202° |
| argument of perigee: | 90.5357° |
| revolutions per day: | 15.75261819 |
| mean anomaly at epoch: | 269.6049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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