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 67479U 26145.41605654 +.00000000 +00000-0 +78738-4 0 00002
2 67479 44.9808 183.2499 0011870 236.0729 123.8976 13.99141842 08
| Epoch (UTC): | 25 May 2026 09:59:07 |
| Eccentricity: | 0.0011870 |
| inclination: | 44.9808° |
| perigee height: | 888 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 183.2499° |
| argument of perigee: | 236.0729° |
| revolutions per day: | 13.99141842 |
| mean anomaly at epoch: | 123.8976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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