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 67356U 26145.34373104 +.00000000 +00000-0 +58399-3 0 00000
2 67356 43.0033 154.4734 0001139 274.8542 85.2179 15.27593156 02
| Epoch (UTC): | 25 May 2026 08:14:58 |
| Eccentricity: | 0.0001139 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.4734° |
| argument of perigee: | 274.8542° |
| revolutions per day: | 15.27593156 |
| mean anomaly at epoch: | 85.2179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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