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 67420U 26145.37439512 +.00000000 +00000-0 +60770-3 0 00007
2 67420 43.0031 164.9711 0001483 243.7397 116.3302 15.27613235 03
| Epoch (UTC): | 25 May 2026 08:59:07 |
| Eccentricity: | 0.0001483 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.9711° |
| argument of perigee: | 243.7397° |
| revolutions per day: | 15.27613235 |
| mean anomaly at epoch: | 116.3302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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