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 63648U 26144.89178501 +.00000000 +00000-0 +92439-3 0 00006
2 63648 42.9996 294.6353 0002321 298.1386 61.9231 15.27601887 02
| Epoch (UTC): | 24 May 2026 21:24:10 |
| Eccentricity: | 0.0002321 |
| inclination: | 42.9996° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 294.6353° |
| argument of perigee: | 298.1386° |
| revolutions per day: | 15.27601887 |
| mean anomaly at epoch: | 61.9231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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