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 67282U 26145.15319772 +.00000000 +00000-0 +22544-3 0 00001
2 67282 97.3931 220.2424 0012226 83.2976 276.9651 15.22763962 02
| Epoch (UTC): | 25 May 2026 03:40:36 |
| Eccentricity: | 0.0012226 |
| inclination: | 97.3931° |
| perigee height: | 489 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 220.2424° |
| argument of perigee: | 83.2976° |
| revolutions per day: | 15.22763962 |
| mean anomaly at epoch: | 276.9651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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