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 64079U 26145.38653674 +.00000000 +00000-0 +60096-3 0 00003
2 64079 42.9992 128.1111 0001354 263.9762 96.0936 15.27592540 09
| Epoch (UTC): | 25 May 2026 09:16:36 |
| Eccentricity: | 0.0001354 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.1111° |
| argument of perigee: | 263.9762° |
| revolutions per day: | 15.27592540 |
| mean anomaly at epoch: | 96.0936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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