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 63118U 26100.30380804 +.00000000 +00000-0 +10368-2 0 00007
2 63118 43.0001 194.0792 0000809 266.6590 93.4169 15.27556691 01
| Epoch (UTC): | 10 April 2026 07:17:29 |
| Eccentricity: | 0.0000809 |
| inclination: | 43.0001° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 194.0792° |
| argument of perigee: | 266.6590° |
| revolutions per day: | 15.27556691 |
| mean anomaly at epoch: | 93.4169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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