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 67039U 26145.53647669 +.00000000 +00000-0 +65661-3 0 00009
2 67039 43.0032 323.9341 0000844 260.2734 99.8022 15.27599859 04
| Epoch (UTC): | 25 May 2026 12:52:31 |
| Eccentricity: | 0.0000844 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 323.9341° |
| argument of perigee: | 260.2734° |
| revolutions per day: | 15.27599859 |
| mean anomaly at epoch: | 99.8022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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