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 64237U 26145.25734036 +.00000000 +00000-0 +12928-2 0 00007
2 64237 43.0004 107.8757 0002315 292.1954 67.8668 15.70878719 07
| Epoch (UTC): | 25 May 2026 06:10:34 |
| Eccentricity: | 0.0002315 |
| inclination: | 43.0004° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 107.8757° |
| argument of perigee: | 292.1954° |
| revolutions per day: | 15.70878719 |
| mean anomaly at epoch: | 67.8668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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