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 63136U 26145.34070546 +.00000000 +00000-0 +12906-2 0 00009
2 63136 43.0022 149.0198 0003033 270.4117 89.6403 15.70872602 03
| Epoch (UTC): | 25 May 2026 08:10:36 |
| Eccentricity: | 0.0003033 |
| inclination: | 43.0022° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 149.0198° |
| argument of perigee: | 270.4117° |
| revolutions per day: | 15.70872602 |
| mean anomaly at epoch: | 89.6403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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