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 63435U 26145.39774037 +.00000000 +00000-0 -10002-2 0 00008
2 63435 53.1581 143.7237 0001617 140.6433 219.4691 15.42231573 04
| Epoch (UTC): | 25 May 2026 09:32:44 |
| Eccentricity: | 0.0001617 |
| inclination: | 53.1581° |
| perigee height: | 438 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 143.7237° |
| argument of perigee: | 140.6433° |
| revolutions per day: | 15.42231573 |
| mean anomaly at epoch: | 219.4691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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