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 67769U 26145.58335647 +.00000000 +00000-0 -11975+0 0 00000
2 67769 51.8954 209.0730 0003804 352.9881 179.9011 15.06595151 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003804 |
| inclination: | 51.8954° |
| perigee height: | 544 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 209.0730° |
| argument of perigee: | 352.9881° |
| revolutions per day: | 15.06595151 |
| mean anomaly at epoch: | 179.9011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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