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 63142U 26145.41477581 +.00000000 +00000-0 +17089-2 0 00001
2 63142 43.0058 147.8230 0002988 258.4475 101.6057 15.70921456 05
| Epoch (UTC): | 25 May 2026 09:57:16 |
| Eccentricity: | 0.0002988 |
| inclination: | 43.0058° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 147.8230° |
| argument of perigee: | 258.4475° |
| revolutions per day: | 15.70921456 |
| mean anomaly at epoch: | 101.6057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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