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 67545U 26145.40494574 +.00000000 +00000-0 +10207-2 0 00007
2 67545 97.2863 32.4987 0001392 89.8127 270.3275 15.33463088 04
| Epoch (UTC): | 25 May 2026 09:43:07 |
| Eccentricity: | 0.0001392 |
| inclination: | 97.2863° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 32.4987° |
| argument of perigee: | 89.8127° |
| revolutions per day: | 15.33463088 |
| mean anomaly at epoch: | 270.3275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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