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 64581U 26145.61168516 +.00000000 +00000-0 +29337-3 0 00006
2 64581 97.7719 260.6105 0004622 76.2074 283.9661 14.95052968 00
| Epoch (UTC): | 25 May 2026 14:40:49 |
| Eccentricity: | 0.0004622 |
| inclination: | 97.7719° |
| perigee height: | 579 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 260.6105° |
| argument of perigee: | 76.2074° |
| revolutions per day: | 14.95052968 |
| mean anomaly at epoch: | 283.9661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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