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 64241U 26145.29968530 +.00000000 +00000-0 +12876-2 0 00006
2 64241 43.0007 107.3193 0001335 258.4266 101.6452 15.70887359 04
| Epoch (UTC): | 25 May 2026 07:11:32 |
| Eccentricity: | 0.0001335 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 107.3193° |
| argument of perigee: | 258.4266° |
| revolutions per day: | 15.70887359 |
| mean anomaly at epoch: | 101.6452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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