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 67033U 26145.19541735 +.00000000 +00000-0 +64280-3 0 00008
2 67033 43.0055 325.6830 0000983 286.1104 73.9639 15.27591066 06
| Epoch (UTC): | 25 May 2026 04:41:24 |
| Eccentricity: | 0.0000983 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 325.6830° |
| argument of perigee: | 286.1104° |
| revolutions per day: | 15.27591066 |
| mean anomaly at epoch: | 73.9639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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