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 64617U 26145.49223198 +.00000000 +00000-0 +70214-3 0 00000
2 64617 53.1605 325.4938 0001615 91.5019 268.6168 15.34407422 07
| Epoch (UTC): | 25 May 2026 11:48:48 |
| Eccentricity: | 0.0001615 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 325.4938° |
| argument of perigee: | 91.5019° |
| revolutions per day: | 15.34407422 |
| mean anomaly at epoch: | 268.6168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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