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 64674U 26145.33422801 +.00000000 +00000-0 +70195-3 0 00006
2 64674 53.1585 129.9775 0001214 94.7266 265.3875 15.34377514 04
| Epoch (UTC): | 25 May 2026 08:01:17 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 129.9775° |
| argument of perigee: | 94.7266° |
| revolutions per day: | 15.34377514 |
| mean anomaly at epoch: | 265.3875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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