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 63401U 26145.40221350 +.00000000 +00000-0 +52244-3 0 00002
2 63401 43.0074 33.7152 0001030 253.2450 106.8289 15.27583153 04
| Epoch (UTC): | 25 May 2026 09:39:11 |
| Eccentricity: | 0.0001030 |
| inclination: | 43.0074° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.7152° |
| argument of perigee: | 253.2450° |
| revolutions per day: | 15.27583153 |
| mean anomaly at epoch: | 106.8289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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