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 68129U 26145.37477425 +.00000000 +00000-0 +75436-4 0 00005
2 68129 50.0009 138.2045 0000217 359.2557 0.8315 13.29330408 01
| Epoch (UTC): | 25 May 2026 08:59:40 |
| Eccentricity: | 0.0000217 |
| inclination: | 50.0009° |
| perigee height: | 1149 km |
| apogee height: | 1149 km |
| right ascension of ascending node: | 138.2045° |
| argument of perigee: | 359.2557° |
| revolutions per day: | 13.29330408 |
| mean anomaly at epoch: | 0.8315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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