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 67048U 26145.55318339 +.00000000 +00000-0 +41768-3 0 00002
2 67048 43.0008 324.0661 0001178 248.1995 111.8731 15.27591912 03
| Epoch (UTC): | 25 May 2026 13:16:35 |
| Eccentricity: | 0.0001178 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.0661° |
| argument of perigee: | 248.1995° |
| revolutions per day: | 15.27591912 |
| mean anomaly at epoch: | 111.8731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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