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 67971U 26144.99939406 +.00000000 +00000-0 +45873-3 0 00009
2 67971 97.2836 155.0272 0001763 106.0382 254.1055 15.33453084 04
| Epoch (UTC): | 24 May 2026 23:59:07 |
| Eccentricity: | 0.0001763 |
| inclination: | 97.2836° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 155.0272° |
| argument of perigee: | 106.0382° |
| revolutions per day: | 15.33453084 |
| mean anomaly at epoch: | 254.1055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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