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 64691U 26145.31592953 +.00000000 +00000-0 +16934-3 0 00000
2 64691 96.0033 271.6821 0010656 284.3018 75.7011 14.72432305 02
| Epoch (UTC): | 25 May 2026 07:34:56 |
| Eccentricity: | 0.0010656 |
| inclination: | 96.0033° |
| perigee height: | 646 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 271.6821° |
| argument of perigee: | 284.3018° |
| revolutions per day: | 14.72432305 |
| mean anomaly at epoch: | 75.7011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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