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 67989U 26145.53774079 +.00000000 +00000-0 +79379-3 0 00000
2 67989 42.9990 335.1677 0000793 280.5101 79.5661 15.27592973 06
| Epoch (UTC): | 25 May 2026 12:54:20 |
| Eccentricity: | 0.0000793 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.1677° |
| argument of perigee: | 280.5101° |
| revolutions per day: | 15.27592973 |
| mean anomaly at epoch: | 79.5661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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