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 67564U 26145.60581123 +.00000000 +00000-0 +57667-3 0 00009
2 67564 97.2857 205.9560 0000579 110.0532 250.0773 15.33448920 01
| Epoch (UTC): | 25 May 2026 14:32:22 |
| Eccentricity: | 0.0000579 |
| inclination: | 97.2857° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9560° |
| argument of perigee: | 110.0532° |
| revolutions per day: | 15.33448920 |
| mean anomaly at epoch: | 250.0773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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