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 68029U 26145.62298777 +.00000000 +00000-0 +67108-3 0 00009
2 68029 97.2845 94.6393 0002406 127.6275 232.5186 15.33454644 04
| Epoch (UTC): | 25 May 2026 14:57:06 |
| Eccentricity: | 0.0002406 |
| inclination: | 97.2845° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.6393° |
| argument of perigee: | 127.6275° |
| revolutions per day: | 15.33454644 |
| mean anomaly at epoch: | 232.5186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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