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 64511U 26144.67875860 +.00000000 +00000-0 +70269-2 0 00000
2 64511 51.8995 250.6462 0000639 43.0121 317.0890 14.76868978 02
| Epoch (UTC): | 24 May 2026 16:17:24 |
| Eccentricity: | 0.0000639 |
| inclination: | 51.8995° |
| perigee height: | 639 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 250.6462° |
| argument of perigee: | 43.0121° |
| revolutions per day: | 14.76868978 |
| mean anomaly at epoch: | 317.0890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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