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 67321U 26145.56867486 +.00000000 +00000-0 +65887-3 0 00007
2 67321 43.0003 251.3501 0001264 276.6664 83.4044 15.27594433 04
| Epoch (UTC): | 25 May 2026 13:38:53 |
| Eccentricity: | 0.0001264 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.3501° |
| argument of perigee: | 276.6664° |
| revolutions per day: | 15.27594433 |
| mean anomaly at epoch: | 83.4044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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