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 64159U 26145.10705938 +.00000000 +00000-0 +31941-3 0 00000
2 64159 97.4530 196.4315 0003768 118.2189 241.9419 15.05682321 01
| Epoch (UTC): | 25 May 2026 02:34:09 |
| Eccentricity: | 0.0003768 |
| inclination: | 97.4530° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 196.4315° |
| argument of perigee: | 118.2189° |
| revolutions per day: | 15.05682321 |
| mean anomaly at epoch: | 241.9419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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