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 63429U 26145.42721157 +.00000000 +00000-0 +20749-3 0 00009
2 63429 54.9896 127.6499 0004412 283.9572 76.0959 15.25084915 08
| Epoch (UTC): | 25 May 2026 10:15:11 |
| Eccentricity: | 0.0004412 |
| inclination: | 54.9896° |
| perigee height: | 488 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 127.6499° |
| argument of perigee: | 283.9572° |
| revolutions per day: | 15.25084915 |
| mean anomaly at epoch: | 76.0959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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