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 67008U 26145.57741443 +.00000000 +00000-0 -19744-3 0 00006
2 67008 70.0044 260.6434 0003164 263.2108 96.8691 14.98319718 09
| Epoch (UTC): | 25 May 2026 13:51:28 |
| Eccentricity: | 0.0003164 |
| inclination: | 70.0044° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.6434° |
| argument of perigee: | 263.2108° |
| revolutions per day: | 14.98319718 |
| mean anomaly at epoch: | 96.8691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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