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 67268U 26145.48420338 +.00000000 +00000-0 +31468-3 0 00007
2 67268 97.3952 220.4504 0016479 86.3112 274.0009 15.22282436 08
| Epoch (UTC): | 25 May 2026 11:37:15 |
| Eccentricity: | 0.0016479 |
| inclination: | 97.3952° |
| perigee height: | 488 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 220.4504° |
| argument of perigee: | 86.3112° |
| revolutions per day: | 15.22282436 |
| mean anomaly at epoch: | 274.0009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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