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 67482U 26145.15193870 +.00000000 +00000-0 +25761-2 0 00005
2 67482 97.3914 222.2155 0005301 105.2151 254.9683 15.43436079 04
| Epoch (UTC): | 25 May 2026 03:38:47 |
| Eccentricity: | 0.0005301 |
| inclination: | 97.3914° |
| perigee height: | 432 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 222.2155° |
| argument of perigee: | 105.2151° |
| revolutions per day: | 15.43436079 |
| mean anomaly at epoch: | 254.9683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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