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 26145.42044602 +.00000000 +00000-0 +68862-3 0 00005
2 63118 43.0010 299.2862 0001448 283.7870 76.2821 15.27591742 08
| Epoch (UTC): | 25 May 2026 10:05:26 |
| Eccentricity: | 0.0001448 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 299.2862° |
| argument of perigee: | 283.7870° |
| revolutions per day: | 15.27591742 |
| mean anomaly at epoch: | 76.2821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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