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 68218U 26145.58939791 +.00000000 +00000-0 +68358-3 0 00000
2 68218 97.2869 21.0390 0001841 93.6444 266.5010 15.33452137 01
| Epoch (UTC): | 25 May 2026 14:08:43 |
| Eccentricity: | 0.0001841 |
| inclination: | 97.2869° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 21.0390° |
| argument of perigee: | 93.6444° |
| revolutions per day: | 15.33452137 |
| mean anomaly at epoch: | 266.5010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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