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 67608U 26145.63555169 +.00000000 +00000-0 +71315-3 0 00008
2 67608 97.2842 210.7176 0000781 109.1266 251.0061 15.33443410 09
| Epoch (UTC): | 25 May 2026 15:15:11 |
| Eccentricity: | 0.0000781 |
| inclination: | 97.2842° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.7176° |
| argument of perigee: | 109.1266° |
| revolutions per day: | 15.33443410 |
| mean anomaly at epoch: | 251.0061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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