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 67408U 26145.35769214 +.00000000 +00000-0 +59763-3 0 00006
2 67408 43.0012 164.8512 0001474 275.2583 84.8100 15.27580533 02
| Epoch (UTC): | 25 May 2026 08:35:04 |
| Eccentricity: | 0.0001474 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.8512° |
| argument of perigee: | 275.2583° |
| revolutions per day: | 15.27580533 |
| mean anomaly at epoch: | 84.8100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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