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 64855U 26145.09477493 +.00000000 +00000-0 +21781-3 0 00004
2 64855 97.4531 0.4314 0002150 83.7024 276.4448 15.05661324 01
| Epoch (UTC): | 25 May 2026 02:16:28 |
| Eccentricity: | 0.0002150 |
| inclination: | 97.4531° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.4314° |
| argument of perigee: | 83.7024° |
| revolutions per day: | 15.05661324 |
| mean anomaly at epoch: | 276.4448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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