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 64856U 26145.12524602 +.00000000 +00000-0 +34899-3 0 00008
2 64856 97.4493 0.5499 0002667 84.2428 275.9103 15.05656817 04
| Epoch (UTC): | 25 May 2026 03:00:21 |
| Eccentricity: | 0.0002667 |
| inclination: | 97.4493° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.5499° |
| argument of perigee: | 84.2428° |
| revolutions per day: | 15.05656817 |
| mean anomaly at epoch: | 275.9103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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