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 63105U 26145.32267492 +.00000000 +00000-0 +15352-2 0 00009
2 63105 42.9972 135.3066 0000661 346.6014 13.4836 15.70860760 06
| Epoch (UTC): | 25 May 2026 07:44:39 |
| Eccentricity: | 0.0000661 |
| inclination: | 42.9972° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 135.3066° |
| argument of perigee: | 346.6014° |
| revolutions per day: | 15.70860760 |
| mean anomaly at epoch: | 13.4836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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