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 67330U 26145.56996061 +.00000000 +00000-0 +55296-3 0 00002
2 67330 43.0001 251.3557 0001265 266.9889 93.0818 15.27585501 07
| Epoch (UTC): | 25 May 2026 13:40:44 |
| Eccentricity: | 0.0001265 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.3557° |
| argument of perigee: | 266.9889° |
| revolutions per day: | 15.27585501 |
| mean anomaly at epoch: | 93.0818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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