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 67477U 26145.45194478 +.00000000 +00000-0 +81459-4 0 00005
2 67477 44.9765 182.6743 0011843 230.2872 129.6918 13.99154202 02
| Epoch (UTC): | 25 May 2026 10:50:48 |
| Eccentricity: | 0.0011843 |
| inclination: | 44.9765° |
| perigee height: | 888 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 182.6743° |
| argument of perigee: | 230.2872° |
| revolutions per day: | 13.99154202 |
| mean anomaly at epoch: | 129.6918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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