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 63269U 26145.63326125 +.00000000 +00000-0 +12119-2 0 00001
2 63269 43.0004 8.1752 0001960 271.3078 88.7565 15.70892463 00
| Epoch (UTC): | 25 May 2026 15:11:53 |
| Eccentricity: | 0.0001960 |
| inclination: | 43.0004° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 8.1752° |
| argument of perigee: | 271.3078° |
| revolutions per day: | 15.70892463 |
| mean anomaly at epoch: | 88.7565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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