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 67840U 26145.51819005 +.00000000 +00000-0 +41653-3 0 00007
2 67840 43.0024 193.1878 0001113 272.4103 87.6621 15.27587484 03
| Epoch (UTC): | 25 May 2026 12:26:11 |
| Eccentricity: | 0.0001113 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.1878° |
| argument of perigee: | 272.4103° |
| revolutions per day: | 15.27587484 |
| mean anomaly at epoch: | 87.6621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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