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 62763U 26145.52168919 +.00000000 +00000-0 +62631-3 0 00007
2 62763 53.1598 325.6392 0001229 90.3284 269.7858 15.31718588 09
| Epoch (UTC): | 25 May 2026 12:31:13 |
| Eccentricity: | 0.0001229 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 325.6392° |
| argument of perigee: | 90.3284° |
| revolutions per day: | 15.31718588 |
| mean anomaly at epoch: | 269.7858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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