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 68216U 26145.39906668 +.00000000 +00000-0 +41436-3 0 00002
2 68216 97.2866 20.8396 0001177 95.8087 264.3290 15.33454025 02
| Epoch (UTC): | 25 May 2026 09:34:39 |
| Eccentricity: | 0.0001177 |
| inclination: | 97.2866° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 20.8396° |
| argument of perigee: | 95.8087° |
| revolutions per day: | 15.33454025 |
| mean anomaly at epoch: | 264.3290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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