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 67789U 26145.58335647 +.00000000 +00000-0 -18528-2 0 00006
2 67789 51.8921 214.2492 0020124 348.9753 132.8327 15.03165115 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0020124 |
| inclination: | 51.8921° |
| perigee height: | 543 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 214.2492° |
| argument of perigee: | 348.9753° |
| revolutions per day: | 15.03165115 |
| mean anomaly at epoch: | 132.8327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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