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 64558U 26145.24275466 +.00000000 +00000-0 +47528-3 0 00004
2 64558 97.4713 261.7159 0004256 228.2764 131.8111 15.26648280 08
| Epoch (UTC): | 25 May 2026 05:49:34 |
| Eccentricity: | 0.0004256 |
| inclination: | 97.4713° |
| perigee height: | 483 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 261.7159° |
| argument of perigee: | 228.2764° |
| revolutions per day: | 15.26648280 |
| mean anomaly at epoch: | 131.8111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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