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 68312U 26145.31561005 +.00000000 +00000-0 +61277-3 0 00008
2 68312 97.2846 271.6629 0001155 67.9657 292.1731 15.75206550 04
| Epoch (UTC): | 25 May 2026 07:34:28 |
| Eccentricity: | 0.0001155 |
| inclination: | 97.2846° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6629° |
| argument of perigee: | 67.9657° |
| revolutions per day: | 15.75206550 |
| mean anomaly at epoch: | 292.1731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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