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 64075U 26145.60374161 +.00000000 +00000-0 +14552-2 0 00000
2 64075 42.9985 354.7070 0001253 277.9572 82.1153 15.70901506 01
| Epoch (UTC): | 25 May 2026 14:29:23 |
| Eccentricity: | 0.0001253 |
| inclination: | 42.9985° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 354.7070° |
| argument of perigee: | 277.9572° |
| revolutions per day: | 15.70901506 |
| mean anomaly at epoch: | 82.1153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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