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 63093U 26145.46775162 +.00000000 +00000-0 +10366-3 0 00009
2 63093 70.0004 160.8295 0004069 270.0615 90.0078 14.98339843 01
| Epoch (UTC): | 25 May 2026 11:13:33 |
| Eccentricity: | 0.0004069 |
| inclination: | 70.0004° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.8295° |
| argument of perigee: | 270.0615° |
| revolutions per day: | 14.98339843 |
| mean anomaly at epoch: | 90.0078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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