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 64382U 26145.54766332 +.00000000 +00000-0 +13948-2 0 00007
2 64382 42.9975 340.9446 0001008 239.9154 120.1614 15.70952599 00
| Epoch (UTC): | 25 May 2026 13:08:38 |
| Eccentricity: | 0.0001008 |
| inclination: | 42.9975° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 340.9446° |
| argument of perigee: | 239.9154° |
| revolutions per day: | 15.70952599 |
| mean anomaly at epoch: | 120.1614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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