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 64544U 26145.55570809 +.00000000 +00000-0 +11868-3 0 00000
2 64544 97.4706 260.6051 0001326 169.9147 190.2115 15.19959691 01
| Epoch (UTC): | 25 May 2026 13:20:13 |
| Eccentricity: | 0.0001326 |
| inclination: | 97.4706° |
| perigee height: | 505 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 260.6051° |
| argument of perigee: | 169.9147° |
| revolutions per day: | 15.19959691 |
| mean anomaly at epoch: | 190.2115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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