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 67296U 26144.77305617 +.00000000 +00000-0 +38682-3 0 00006
2 67296 97.3946 220.1807 0010250 82.9396 277.3007 15.24680888 01
| Epoch (UTC): | 24 May 2026 18:33:12 |
| Eccentricity: | 0.0010250 |
| inclination: | 97.3946° |
| perigee height: | 485 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 220.1807° |
| argument of perigee: | 82.9396° |
| revolutions per day: | 15.24680888 |
| mean anomaly at epoch: | 277.3007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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