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 63831U 26145.25435267 +.00000000 +00000-0 +58214-3 0 00009
2 63831 43.0023 100.2009 0001167 260.8128 99.2592 15.27584792 05
| Epoch (UTC): | 25 May 2026 06:06:16 |
| Eccentricity: | 0.0001167 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2009° |
| argument of perigee: | 260.8128° |
| revolutions per day: | 15.27584792 |
| mean anomaly at epoch: | 99.2592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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