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 67920U 26145.42352823 +.00000000 +00000-0 +35742-3 0 00008
2 67920 43.0002 172.2511 0001550 276.4678 83.5997 15.27588716 06
| Epoch (UTC): | 25 May 2026 10:09:52 |
| Eccentricity: | 0.0001550 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 172.2511° |
| argument of perigee: | 276.4678° |
| revolutions per day: | 15.27588716 |
| mean anomaly at epoch: | 83.5997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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