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 64887U 26145.59047367 +.00000000 +00000-0 +70537-3 0 00000
2 64887 97.4489 115.5473 0004833 224.0031 136.0829 15.36992406 06
| Epoch (UTC): | 25 May 2026 14:10:16 |
| Eccentricity: | 0.0004833 |
| inclination: | 97.4489° |
| perigee height: | 452 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 115.5473° |
| argument of perigee: | 224.0031° |
| revolutions per day: | 15.36992406 |
| mean anomaly at epoch: | 136.0829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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