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 67404U 26145.47817569 +.00000000 +00000-0 +44505-3 0 00000
2 67404 43.0003 164.0389 0001447 272.9432 87.1254 15.27586269 07
| Epoch (UTC): | 25 May 2026 11:28:34 |
| Eccentricity: | 0.0001447 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.0389° |
| argument of perigee: | 272.9432° |
| revolutions per day: | 15.27586269 |
| mean anomaly at epoch: | 87.1254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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