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 67470U 26145.38354292 +.00000000 +00000-0 +67290-3 0 00008
2 67470 43.0004 131.9028 0001421 267.2862 92.7827 15.27594250 07
| Epoch (UTC): | 25 May 2026 09:12:18 |
| Eccentricity: | 0.0001421 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.9028° |
| argument of perigee: | 267.2862° |
| revolutions per day: | 15.27594250 |
| mean anomaly at epoch: | 92.7827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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