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 63823U 26145.27394339 +.00000000 +00000-0 +63655-3 0 00001
2 63823 43.0013 95.9882 0001430 260.4643 99.6047 15.27600981 03
| Epoch (UTC): | 25 May 2026 06:34:28 |
| Eccentricity: | 0.0001430 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 95.9882° |
| argument of perigee: | 260.4643° |
| revolutions per day: | 15.27600981 |
| mean anomaly at epoch: | 99.6047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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