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 67506U 26145.56865447 +.00000000 +00000-0 +68300-3 0 00000
2 67506 42.9984 239.8646 0001382 277.9514 82.1181 15.27590192 01
| Epoch (UTC): | 25 May 2026 13:38:51 |
| Eccentricity: | 0.0001382 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.8646° |
| argument of perigee: | 277.9514° |
| revolutions per day: | 15.27590192 |
| mean anomaly at epoch: | 82.1181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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