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 64099U 26145.40235682 +.00000000 +00000-0 +49257-3 0 00009
2 64099 53.1621 30.7192 0001278 84.2374 275.8772 15.30212895 00
| Epoch (UTC): | 25 May 2026 09:39:23 |
| Eccentricity: | 0.0001278 |
| inclination: | 53.1621° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.7192° |
| argument of perigee: | 84.2374° |
| revolutions per day: | 15.30212895 |
| mean anomaly at epoch: | 275.8772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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