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 63082U 26145.47628755 +.00000000 +00000-0 +40413-3 0 00009
2 63082 70.0007 160.8540 0004071 263.0938 96.9758 14.98333978 01
| Epoch (UTC): | 25 May 2026 11:25:51 |
| Eccentricity: | 0.0004071 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.8540° |
| argument of perigee: | 263.0938° |
| revolutions per day: | 14.98333978 |
| mean anomaly at epoch: | 96.9758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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