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 67283U 26144.77640558 +.00000000 +00000-0 +23749-3 0 00006
2 67283 97.3939 220.0007 0011967 84.0248 276.2353 15.23567532 06
| Epoch (UTC): | 24 May 2026 18:38:01 |
| Eccentricity: | 0.0011967 |
| inclination: | 97.3939° |
| perigee height: | 487 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 220.0007° |
| argument of perigee: | 84.0248° |
| revolutions per day: | 15.23567532 |
| mean anomaly at epoch: | 276.2353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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