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 68334U 26145.56182689 +.00000000 +00000-0 +55161-3 0 00001
2 68334 53.1600 351.3149 0001522 87.4157 272.7018 15.30213089 08
| Epoch (UTC): | 25 May 2026 13:29:01 |
| Eccentricity: | 0.0001522 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.3149° |
| argument of perigee: | 87.4157° |
| revolutions per day: | 15.30213089 |
| mean anomaly at epoch: | 272.7018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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