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 67104U 26145.19072054 +.00000000 +00000-0 +96147-3 0 00007
2 67104 43.0040 97.1615 0003175 243.7321 116.3205 15.27598085 06
| Epoch (UTC): | 25 May 2026 04:34:38 |
| Eccentricity: | 0.0003175 |
| inclination: | 43.0040° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 97.1615° |
| argument of perigee: | 243.7321° |
| revolutions per day: | 15.27598085 |
| mean anomaly at epoch: | 116.3205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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