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 63839U 26145.32634505 +.00000000 +00000-0 +46291-3 0 00003
2 63839 43.0017 5.0240 0001003 265.5019 94.5718 15.27591346 06
| Epoch (UTC): | 25 May 2026 07:49:56 |
| Eccentricity: | 0.0001003 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.0240° |
| argument of perigee: | 265.5019° |
| revolutions per day: | 15.27591346 |
| mean anomaly at epoch: | 94.5718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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