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 63141U 26145.36711097 +.00000000 +00000-0 +13094-2 0 00009
2 63141 43.0006 148.3373 0005815 243.0909 116.9365 15.70976527 05
| Epoch (UTC): | 25 May 2026 08:48:38 |
| Eccentricity: | 0.0005815 |
| inclination: | 43.0006° |
| perigee height: | 352 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 148.3373° |
| argument of perigee: | 243.0909° |
| revolutions per day: | 15.70976527 |
| mean anomaly at epoch: | 116.9365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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