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 63285U 26145.51110625 +.00000000 +00000-0 +50569-3 0 00004
2 63285 43.0024 167.8121 0001920 273.8271 86.2361 15.27595058 00
| Epoch (UTC): | 25 May 2026 12:15:59 |
| Eccentricity: | 0.0001920 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.8121° |
| argument of perigee: | 273.8271° |
| revolutions per day: | 15.27595058 |
| mean anomaly at epoch: | 86.2361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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