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 63039U 26145.33335647 +.00000000 +00000-0 +13917-2 0 00009
2 63039 53.1581 262.2558 0001184 98.7763 109.6823 15.30209787 01
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001184 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 262.2558° |
| argument of perigee: | 98.7763° |
| revolutions per day: | 15.30209787 |
| mean anomaly at epoch: | 109.6823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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