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 64168U 26145.12645587 +.00000000 +00000-0 -19585-3 0 00006
2 64168 97.4525 196.5620 0001926 138.6154 221.5219 15.05647530 02
| Epoch (UTC): | 25 May 2026 03:02:05 |
| Eccentricity: | 0.0001926 |
| inclination: | 97.4525° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.5620° |
| argument of perigee: | 138.6154° |
| revolutions per day: | 15.05647530 |
| mean anomaly at epoch: | 221.5219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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