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 67928U 26145.45936120 +.00000000 +00000-0 +32349-3 0 00007
2 67928 43.0024 171.6486 0001351 274.1595 85.9102 15.27582372 00
| Epoch (UTC): | 25 May 2026 11:01:28 |
| Eccentricity: | 0.0001351 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.6486° |
| argument of perigee: | 274.1595° |
| revolutions per day: | 15.27582372 |
| mean anomaly at epoch: | 85.9102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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