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 67495U 26145.55081563 +.00000000 +00000-0 +75783-3 0 00008
2 67495 42.9987 240.6136 0000609 256.8917 103.1866 15.27603275 00
| Epoch (UTC): | 25 May 2026 13:13:10 |
| Eccentricity: | 0.0000609 |
| inclination: | 42.9987° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 240.6136° |
| argument of perigee: | 256.8917° |
| revolutions per day: | 15.27603275 |
| mean anomaly at epoch: | 103.1866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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