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 63083U 26145.48028711 +.00000000 +00000-0 +30756-3 0 00006
2 63083 70.0004 160.8761 0003798 273.6305 86.4419 14.98326923 04
| Epoch (UTC): | 25 May 2026 11:31:36 |
| Eccentricity: | 0.0003798 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.8761° |
| argument of perigee: | 273.6305° |
| revolutions per day: | 14.98326923 |
| mean anomaly at epoch: | 86.4419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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