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 67936U 26145.61620774 +.00000000 +00000-0 +36746-3 0 00004
2 67936 42.9989 116.4672 0000957 270.4253 89.6489 15.27590564 03
| Epoch (UTC): | 25 May 2026 14:47:20 |
| Eccentricity: | 0.0000957 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 116.4672° |
| argument of perigee: | 270.4253° |
| revolutions per day: | 15.27590564 |
| mean anomaly at epoch: | 89.6489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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