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 64413U 26145.37705706 +.00000000 +00000-0 -11685-5 0 00001
2 64413 70.0006 241.1248 0003489 268.7587 91.3173 14.98340947 05
| Epoch (UTC): | 25 May 2026 09:02:57 |
| Eccentricity: | 0.0003489 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 241.1248° |
| argument of perigee: | 268.7587° |
| revolutions per day: | 14.98340947 |
| mean anomaly at epoch: | 91.3173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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