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 67940U 26145.33281367 +.00000000 +00000-0 +44757-3 0 00000
2 67940 42.9988 117.7601 0001419 268.8445 91.2244 15.27586684 07
| Epoch (UTC): | 25 May 2026 07:59:15 |
| Eccentricity: | 0.0001419 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 117.7601° |
| argument of perigee: | 268.8445° |
| revolutions per day: | 15.27586684 |
| mean anomaly at epoch: | 91.2244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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