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 64167U 26145.13477146 +.00000000 +00000-0 -98141-3 0 00005
2 64167 97.4512 196.5484 0001816 162.3477 197.7814 15.05617350 07
| Epoch (UTC): | 25 May 2026 03:14:04 |
| Eccentricity: | 0.0001816 |
| inclination: | 97.4512° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.5484° |
| argument of perigee: | 162.3477° |
| revolutions per day: | 15.05617350 |
| mean anomaly at epoch: | 197.7814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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