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 63761U 26145.53524966 +.00000000 +00000-0 +11559-2 0 00007
2 63761 43.0008 188.8341 0001325 263.3864 96.6852 15.70869248 02
| Epoch (UTC): | 25 May 2026 12:50:45 |
| Eccentricity: | 0.0001325 |
| inclination: | 43.0008° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 188.8341° |
| argument of perigee: | 263.3864° |
| revolutions per day: | 15.70869248 |
| mean anomaly at epoch: | 96.6852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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