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 64190U 26145.11547264 +.00000000 +00000-0 +39331-3 0 00003
2 64190 53.1607 96.3200 0001081 100.4879 259.6243 15.30204472 02
| Epoch (UTC): | 25 May 2026 02:46:16 |
| Eccentricity: | 0.0001081 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 96.3200° |
| argument of perigee: | 100.4879° |
| revolutions per day: | 15.30204472 |
| mean anomaly at epoch: | 259.6243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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