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 64861U 26145.56552493 +.00000000 +00000-0 +12478-3 0 00000
2 64861 97.4517 0.8936 0002348 87.1390 273.0106 15.05654472 09
| Epoch (UTC): | 25 May 2026 13:34:21 |
| Eccentricity: | 0.0002348 |
| inclination: | 97.4517° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.8936° |
| argument of perigee: | 87.1390° |
| revolutions per day: | 15.05654472 |
| mean anomaly at epoch: | 273.0106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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