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 67265U 26145.45410632 +.00000000 +00000-0 +36919-3 0 00003
2 67265 97.3936 220.4767 0016143 86.5990 273.7093 15.22895441 07
| Epoch (UTC): | 25 May 2026 10:53:54 |
| Eccentricity: | 0.0016143 |
| inclination: | 97.3936° |
| perigee height: | 486 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 220.4767° |
| argument of perigee: | 86.5990° |
| revolutions per day: | 15.22895441 |
| mean anomaly at epoch: | 273.7093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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