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 67307U 26145.62249801 +.00000000 +00000-0 +57484-3 0 00007
2 67307 43.0013 250.8925 0001548 256.3098 103.7581 15.27595410 02
| Epoch (UTC): | 25 May 2026 14:56:23 |
| Eccentricity: | 0.0001548 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.8925° |
| argument of perigee: | 256.3098° |
| revolutions per day: | 15.27595410 |
| mean anomaly at epoch: | 103.7581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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