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 64350U 26145.55167380 +.00000000 +00000-0 +18538-3 0 00002
2 64350 70.0008 200.7138 0003831 267.4028 92.6693 14.98334610 04
| Epoch (UTC): | 25 May 2026 13:14:24 |
| Eccentricity: | 0.0003831 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 200.7138° |
| argument of perigee: | 267.4028° |
| revolutions per day: | 14.98334610 |
| mean anomaly at epoch: | 92.6693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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