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 64546U 26145.58490557 +.00000000 +00000-0 +28434-3 0 00003
2 64546 97.4661 261.4613 0000782 129.0996 231.0311 15.23770640 02
| Epoch (UTC): | 25 May 2026 14:02:15 |
| Eccentricity: | 0.0000782 |
| inclination: | 97.4661° |
| perigee height: | 494 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 261.4613° |
| argument of perigee: | 129.0996° |
| revolutions per day: | 15.23770640 |
| mean anomaly at epoch: | 231.0311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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