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 63049U 26144.65347951 +.00000000 +00000-0 +13845-3 0 00006
2 63049 53.1595 277.6071 0001222 89.7414 270.3729 15.34378215 01
| Epoch (UTC): | 24 May 2026 15:41:00 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 277.6071° |
| argument of perigee: | 89.7414° |
| revolutions per day: | 15.34378215 |
| mean anomaly at epoch: | 270.3729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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