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 67942U 26145.27898847 +.00000000 +00000-0 +44909-3 0 00001
2 67942 42.9985 118.2100 0001443 272.7177 87.3509 15.27592837 06
| Epoch (UTC): | 25 May 2026 06:41:44 |
| Eccentricity: | 0.0001443 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.2100° |
| argument of perigee: | 272.7177° |
| revolutions per day: | 15.27592837 |
| mean anomaly at epoch: | 87.3509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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