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 67921U 26145.55044723 +.00000000 +00000-0 +49927-3 0 00000
2 67921 43.0007 171.4919 0001302 265.0246 95.0457 15.27598155 02
| Epoch (UTC): | 25 May 2026 13:12:38 |
| Eccentricity: | 0.0001302 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.4919° |
| argument of perigee: | 265.0246° |
| revolutions per day: | 15.27598155 |
| mean anomaly at epoch: | 95.0457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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