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 63729U 26145.36084461 +.00000000 +00000-0 +14466-3 0 00004
2 63729 51.9005 129.0662 0000889 5.8548 354.2425 14.79931825 04
| Epoch (UTC): | 25 May 2026 08:39:36 |
| Eccentricity: | 0.0000889 |
| inclination: | 51.9005° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 129.0662° |
| argument of perigee: | 5.8548° |
| revolutions per day: | 14.79931825 |
| mean anomaly at epoch: | 354.2425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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