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 64355U 26145.40980538 +.00000000 +00000-0 +20245-3 0 00007
2 64355 70.0008 201.0225 0003656 268.2994 91.7746 14.98334916 04
| Epoch (UTC): | 25 May 2026 09:50:07 |
| Eccentricity: | 0.0003656 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.0225° |
| argument of perigee: | 268.2994° |
| revolutions per day: | 14.98334916 |
| mean anomaly at epoch: | 91.7746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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