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 67612U 26145.45607684 +.00000000 +00000-0 +44510-3 0 00000
2 67612 97.2851 210.6544 0000258 132.7449 227.3815 15.33453812 06
| Epoch (UTC): | 25 May 2026 10:56:45 |
| Eccentricity: | 0.0000258 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.6544° |
| argument of perigee: | 132.7449° |
| revolutions per day: | 15.33453812 |
| mean anomaly at epoch: | 227.3815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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