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 67816U 26145.41758784 +.00000000 +00000-0 +49376-3 0 00005
2 67816 97.2860 333.5711 0001972 68.5087 291.6366 15.33462799 00
| Epoch (UTC): | 25 May 2026 10:01:19 |
| Eccentricity: | 0.0001972 |
| inclination: | 97.2860° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.5711° |
| argument of perigee: | 68.5087° |
| revolutions per day: | 15.33462799 |
| mean anomaly at epoch: | 291.6366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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