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 68209U 26145.22235919 +.00000000 +00000-0 +10685-2 0 00001
2 68209 97.2873 20.6207 0001931 81.2651 278.8811 15.33431930 04
| Epoch (UTC): | 25 May 2026 05:20:11 |
| Eccentricity: | 0.0001931 |
| inclination: | 97.2873° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.6207° |
| argument of perigee: | 81.2651° |
| revolutions per day: | 15.33431930 |
| mean anomaly at epoch: | 278.8811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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