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 67030U 26145.49036938 +.00000000 +00000-0 +70201-3 0 00002
2 67030 42.9964 324.4588 0000590 243.4840 116.5951 15.27598318 02
| Epoch (UTC): | 25 May 2026 11:46:07 |
| Eccentricity: | 0.0000590 |
| inclination: | 42.9964° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 324.4588° |
| argument of perigee: | 243.4840° |
| revolutions per day: | 15.27598318 |
| mean anomaly at epoch: | 116.5951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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