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 67811U 26145.09674852 +.00000000 +00000-0 +47869-3 0 00002
2 67811 97.2847 333.2425 0000985 102.8204 257.3149 15.33454506 00
| Epoch (UTC): | 25 May 2026 02:19:19 |
| Eccentricity: | 0.0000985 |
| inclination: | 97.2847° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 333.2425° |
| argument of perigee: | 102.8204° |
| revolutions per day: | 15.33454506 |
| mean anomaly at epoch: | 257.3149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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