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 67561U 26145.44267094 +.00000000 +00000-0 +41451-3 0 00000
2 67561 97.2856 205.7199 0000145 114.0809 246.0449 15.33454032 09
| Epoch (UTC): | 25 May 2026 10:37:26 |
| Eccentricity: | 0.0000145 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.7199° |
| argument of perigee: | 114.0809° |
| revolutions per day: | 15.33454032 |
| mean anomaly at epoch: | 246.0449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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