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 64100U 26145.40024382 +.00000000 +00000-0 +42934-3 0 00000
2 64100 53.1614 30.7069 0000981 91.0505 269.0608 15.30210289 08
| Epoch (UTC): | 25 May 2026 09:36:21 |
| Eccentricity: | 0.0000981 |
| inclination: | 53.1614° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.7069° |
| argument of perigee: | 91.0505° |
| revolutions per day: | 15.30210289 |
| mean anomaly at epoch: | 269.0608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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