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 64165U 26145.55013747 +.00000000 +00000-0 +56160-3 0 00006
2 64165 97.4451 196.9113 0001832 125.4290 234.7108 15.05667553 09
| Epoch (UTC): | 25 May 2026 13:12:11 |
| Eccentricity: | 0.0001832 |
| inclination: | 97.4451° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.9113° |
| argument of perigee: | 125.4290° |
| revolutions per day: | 15.05667553 |
| mean anomaly at epoch: | 234.7108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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