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 68134U 26145.24946666 +.00000000 +00000-0 +84163-4 0 00002
2 68134 50.0052 138.2462 0000528 349.5189 10.5672 13.29331933 04
| Epoch (UTC): | 25 May 2026 05:59:13 |
| Eccentricity: | 0.0000528 |
| inclination: | 50.0052° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 138.2462° |
| argument of perigee: | 349.5189° |
| revolutions per day: | 13.29331933 |
| mean anomaly at epoch: | 10.5672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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