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 67263U 26145.45202848 +.00000000 +00000-0 +35834-3 0 00004
2 67263 97.3957 220.5200 0016197 85.8280 274.4808 15.22951329 04
| Epoch (UTC): | 25 May 2026 10:50:55 |
| Eccentricity: | 0.0016197 |
| inclination: | 97.3957° |
| perigee height: | 486 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 220.5200° |
| argument of perigee: | 85.8280° |
| revolutions per day: | 15.22951329 |
| mean anomaly at epoch: | 274.4808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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