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 67038U 26145.53134263 +.00000000 +00000-0 +65069-3 0 00001
2 67038 43.0017 323.9004 0001079 279.5239 80.5490 15.27588500 03
| Epoch (UTC): | 25 May 2026 12:45:08 |
| Eccentricity: | 0.0001079 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 323.9004° |
| argument of perigee: | 279.5239° |
| revolutions per day: | 15.27588500 |
| mean anomaly at epoch: | 80.5490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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