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 64309U 26145.30335237 +.00000000 +00000-0 +41752-3 0 00001
2 64309 70.0017 1.3176 0002837 269.8494 90.2340 14.98328030 05
| Epoch (UTC): | 25 May 2026 07:16:49 |
| Eccentricity: | 0.0002837 |
| inclination: | 70.0017° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3176° |
| argument of perigee: | 269.8494° |
| revolutions per day: | 14.98328030 |
| mean anomaly at epoch: | 90.2340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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